ExoMars 2018 MGSE General Design Requirements ...emits.sso.esa.int/emits-doc/ALENIA/Exomars/ExoMars_Mission_2018/... · 2018 Mission System Engineering Manager ... the procurement

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EXM-M2-SSR-AI-0033 14 June 2013

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THALES ALENIA SPACE INTERNAL

This document is not to be reproduced, modified, adapted, published, translated in any material form in whole or in part nor disclosed to any third party without the prior written permission of Thales Alenia Space.

2013, Thales Alenia Space Template 83230326-DOC-TAS-EN/002

ExoMars 2018

MGSE General Design Requirements Specification

DRL/DRD: AV-16 W.P. No: EB20-1BA

Written by Responsibility + handwritten signature if no electronic workflow tool

Author

Verified by

Checker

Product Assurance Manager

Configuration Control Manager

AIT Manager

2018 Mission System Engineering Manager

Approved by

ExoMars Deputy and 2018 Mission Program Manager

ExoMars Program Director

Documentation Manager

Approval evidence is kept within the documentation management system.

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CHANGE RECORDS

ISSUE DATE § CHANGE RECORDS AUTHOR

01 14 June 2013

First Release R.MORONI

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TABLE OF CONTENTS

1. SCOPE AND APPLICABILITY ........................... .................................................................................. 7

2. DOCUMENTS ........................................................................................................................................ 8

2.1 ESA Informative Documents ......................... ........................................................................................... 8

2.2 TAS-I Normative Documents ......................... ........................................................................................... 8

2.3 TAS-I Informative Documents ....................... ........................................................................................... 9

2.4 Local Reference Documents ......................... ........................................................................................... 9

3. ACRONYMS ........................................................................................................................................ 10

4. UTILISATION AND MISSION ........................... .................................................................................. 11

4.1 Mechanical Ground Support Equipment Definition .... ......................................................................... 11

4.2 MGSE Items ........................................ ...................................................................................................... 11

5. GENERAL PERFORMANCE REQUIREMENTS .................. ............................................................. 14

5.1 Items Standardization ............................. ................................................................................................ 14

5.2 Interface Design................................... .................................................................................................... 14

5.3 Handling/Hoisting ................................. ................................................................................................... 17

5.4 Stability ......................................... ............................................................................................................ 17

5.5 Parking ........................................... .......................................................................................................... 18

5.6 Displacements ..................................... .................................................................................................... 18

5.7 Life Time ......................................... .......................................................................................................... 18

5.8 Maintainability.................................... ...................................................................................................... 19 5.8.1 First Line Maintenance .......................................................................................................................... 21 5.8.2 Spare Parts ........................................................................................................................................... 21 5.8.3 Accessibility ........................................................................................................................................... 22 5.8.4 Standardization ..................................................................................................................................... 22

5.9 Transportability .................................. ..................................................................................................... 23

5.10 Nameplates and Product Marking .................... ..................................................................................... 24

5.11 Workmanship ....................................... .................................................................................................... 25

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6. INTERFACE REQUIREMENTS .......................................................................................................... 26

6.1 MGSE to F/H Interfaces ............................ ............................................................................................... 26

6.2 MGSE to Facilities Interfaces ..................... ............................................................................................ 26

6.3 MGSE to Transportation Means Interfaces ........... ................................................................................ 30

7. DESIGN AND CONSTRUCTION REQUIREMENTS ......................................................................... 32

7.1 General Design Requirements ....................... ........................................................................................ 32

7.2 Mechanical Design ................................. ................................................................................................. 32 7.2.1 Attenuation System Requirements ....................................................................................................... 35

7.3 Parts, Materials and Processes .................... ......................................................................................... 37 7.3.1 Materials ................................................................................................................................................ 37 7.3.2 Processes ............................................................................................................................................. 42

7.4 Electrical Design ................................. .................................................................................................... 44 7.4.1 Electrical and Electronic Safety Criteria ................................................................................................ 44 7.4.2 Grounding and Bonding Safety Criteria ................................................................................................ 47 7.4.3 Cable and Wiring Safety Criteria ........................................................................................................... 49 7.4.4 Connector and Switch Safety Criteria ................................................................................................... 50 7.4.5 Overload Protection .............................................................................................................................. 51

8. ENVIRONMENTAL REQUIREMENT ......................... ........................................................................ 53

8.1 Integration and Test Facility Environment ......... .................................................................................. 53

8.2 Storage in External Environment.................... ....................................................................................... 54

8.3 Transport Environment ............................. .............................................................................................. 55

8.4 On-Ground Mechanical Environment .................. .................................................................................. 56 8.4.1 Design Load Factors ............................................................................................................................. 56 8.4.2 Dynamic Loads ..................................................................................................................................... 57

9. PRODUCT ASSURANCE REQUIREMENTS .................... ................................................................ 59

9.1 PA Safety Standard Requirements ................... ..................................................................................... 59

9.2 Reliability Requirements .......................... .............................................................................................. 59

9.3 Safety Factors .................................... ...................................................................................................... 60

9.4 Safety and Human Engineering ...................... ....................................................................................... 60 9.4.1 Safety Mechanical Requirements ......................................................................................................... 60 9.4.2 Hazard Control & Human Factor Requirements ................................................................................... 63

9.5 Cleanliness ....................................... ........................................................................................................ 69

10. VERIFICATION REQUIREMENTS ................................................................................................. 72

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10.1 Acceptance Verification ........................... ............................................................................................... 72

10.2 Verification Methods .............................. ................................................................................................. 72 10.2.1 Review of Design .............................................................................................................................. 72 10.2.2 Analysis............................................................................................................................................. 72 10.2.3 Inspection ......................................................................................................................................... 73 10.2.4 Test ................................................................................................................................................... 73

10.2.4.1 Acceptance Test Description ................................................................................................... 74

11. DOCUMENTATION ......................................................................................................................... 77

12. PREPARATION FOR DELIVERY........................... ........................................................................ 78

12.1 MGSE Shipping and Reusable Container .............. ............................................................................... 78

12.2 Shipping and Reusable Container Design Performances .................................................................. 79

12.3 Shipping and Reusable Container Provisions ........ ............................................................................. 80

12.4 Shipping and Reusable Containers Marking .......... .............................................................................. 82

13. PLANETARY PROTECTION IMPLEMENTATION REQUIREMENTS .. ....................................... 84

13.1 Introduction ...................................... ........................................................................................................ 84

13.2 PP Requirements for MGSE to be introduced in the IS O 7HC Clean Room .................................. ... 84

13.3 PP Requirements for MGSE to be introduced in the IS O 3 AMC-9 Clean Room .............................. 86

14. ANNEX 1: EXM-M2-SSR-AI-0033 VERSUS ALD MGSE APPLIC ABILITY MATRIX ................. 89

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TABLE OF ANNEXES

NONE

LIST OF FIGURES

Figure 6.2-1: I/F to EDU .............................................................................................................................................. 29

Figure 6.3-1 : Cargo Bay Dimensions of Antonov AN-124 ......................................................................................... 31

LIST OF TABLES

Table 7-1 : MGSE Design and Proof Safety Factors .................................................................................................. 34

Table 7-2 : Sinusoidal and Random Acceleration Combination Method .................................................................... 36

Table 7-3 : Compatible Galvanic Couples .................................................................................................................. 41

Table 8-1 : MGSE Quasistatic Load Factors .............................................................................................................. 56

Table 8-2 : Sinusoidal Acceleration Input ................................................................................................................... 57

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1. SCOPE AND APPLICABILITY

The purpose of this document is to establish the general requirements for the design of the Ground Support Equipment (MGSE and FGSE) procured by TAS-I for the ALD AIT activities for the Mission 2018 of the ExoMars Spacecraft program. Moreover it provides general requirements for the design of MGSE provided by other sub-contractors and used by TAS-I for assembly, integration, transportation and test activities at Module and Spacecraft Composite (SCC) system level.

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2. DOCUMENTS

Documents in the following listed are directly derived from the official ExoMars nomenclature as for EXM-M2-LIS-AI-0059, “List of NR/IR documents, acronyms and abbreviations". This specification responds to the applicable requirements contained in the ESA “ExoMars 2018 Assembly, Integration and Verification Requirements”, EXM-MS-RSD-ESA-00031 (currently in draft version), and its references, that are totally reflected inside this document. At the same way, the ESA IR documents reported below are intended to inform the Agency on the documentation used to prepare this specification and are not applicable nor provided to the Subcontractors. The general requirements relevant to MGSE and FGSE contained in such IR documents have been included in this specification. Reference Documents listed in the below paragraphs are provided to the Subcontractors responsible of the procurement of the Analytical Laboratory Drawer (ALD) MGSE and FGSE and of the ones provided by other sub-contractors and used by TAS-I for assembly, integration, transportation and test activities at Module and Spacecraft Composite (SCC) system level. A complete list of the documents used inside the ExoMars project is provided in [IR 05002], EXM-M2-LIS-AI-0059: “List of NR/IR documents, acronyms and abbreviations".

2.1 ESA Informative Documents

[IR 020] Configuration and Document Management Requirements EXM-MS-RS-ESA-00008 [IR 18002] ExoMars 2018 Assenbly, Integration and Verification

Requirements EXM-M2-RSD-ESA-00031 (Unsigned)

[IR 18007] ExoMars 2018 Product Assurance Requirements EXM-M2-RSD-ESA-00030 (Unsigned)

[ES 104] Particles Contamination Monitoring for Spacecraft Systems and Cleanrooms

ECSS-Q-ST-70-50C

All other ESA Informative Documents - not applicable

2.2 TAS-I Normative Documents

[NR 0199] ExoMars CADM Rules EXM-MS-RQM-AI-0024

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2.3 TAS-I Informative Documents

[IR 0112] PA requirements for Subcontractors EXM-MS-RQM-AI-0004 [IR 05008] ExoMars 2018 PA requirements for Subcontractors EXM-M2-RQM-AI-0067 [IR 05011] ExoMars 2018 Planetary Protection Implementation

Requirements EXM-M2-SSR-AI-0031

[IR 0424] ALD Mechanical ICD (MICD) EXM-RM-ICD-AI-0040 [IR 0443] Rover Module Mechanical ICD (MICD) EXM-RM-ICD-AI-0043 [IR 05014] ExoMars 2018 Cleanliness & Contamination

Requirements Specification EXM-M2-SSR-AI-0030

[IR 0438] ExoMars RM Cleanliness and Contamination Control Requirements

EXM-RM-SSR-AI-0015

[IR 05002] ExoMars 2018 List of NR/IR Documents, Acronims and Abbreviations

EXM-M2-LIS-AI-0059

NOTE: The [IR 0112] is applicable only to the MGSE of the Rover Module and the Analytical Laboratory Drawer (ALD), while for the MGSE of all other modules the [IR 05008] is the applicable one.

2.4 Local Reference Documents

[RD 01] Space Shuttle Payload Ground Safety Handbook KHB 1700.7C [RD 02] Direttiva relativa alle macchine che modifica la direttiva

95/16/CE (rifusione della Dir. 98/37/CE) Directive 2006/42/CE of UE

[RD 03] Testo Unico sulla salute e sicurezza sul lavoro Decreto Legislativo N. 81 del 09/04/2008

[RD 04] Human Engineering Design Criteria for Military Systems, Equipment and Facilities

MIL-STD-1472C

[RD 05] Cleanrooms and Associated Controlled Environment ISO 14644 [RD 06] Electromagnetic Compatibility (EMC) Directive 2004/108/EEC [RD 07] Direttiva 2006/95/CE relativa al materiale elettrico

destinato ad essere adoperato entro taluni limiti di tensione

Directive 2006/95/EEC

[RD 08] International Standards for Phytosanitary Measures ISPM 15 [RD 09] "Pressure Equalization Requirements for Aircraft and

Shipping Containers" IATA ICAO International Standard Association 80/2

[RD 10] Law concerning equipment intended for use in potentially explosive atmospheres

Directive ATEX 94/9/EC

[RD 11] Test Method Standard MIL-STD-810G [RD 12] CSG Safety Regulations - General Rules - vol.1 CSG-RS-10A-CN [RD 13] CSG Safety Regulations - Specific Rules Ground

Installations - vol.2 part 1 CSG-RS-21A-CN

[RD A106] Flammability, Odor & Out gassing Requirements NASA-STD-6001 [RD A111] Preservation, Storage, Handling and Transportation of

ESA spacecraft hardware PSS-01-202

[RD A130] Standard for Lifting devices and Equipment - Change 1 NASA-STD-8719.9 NOTE: The MGSE safety and proof factors requirements defined in the [NR A130] and [RD 01] are covering the relevant ones of the [RD 12] and [RD 13].

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3. ACRONYMS

For the acronyms list refer to [NR 05002].

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4. UTILISATION AND MISSION

4.1 Mechanical Ground Support Equipment Definition

The Mechanical Ground Support Equipment (MGSE) consists exclusively of non-flight devices for mechanical support in the integration, test, hoisting/handling/storage and shipping activities. MGSE includes all necessary mechanical equipment used to operate on unit, subsystem, module and spacecraft at AIT system level as well as at launch operations level. MGSE shall be compliant with all duties related to its function as part of the ExoMars program.

4.2 MGSE Items

This general specification shall be applicable either to the ExoMars MGSE procured by TAS-I or those delivered to TAS-I by other space segment element contractors (e.g. of Rover, Carrier, etc..). The list of the used MGSE, reported in the following paragraphs, includes the following categories:

• Handling and Integration Devices (including Interface Adapters) • Transport and Storage Containers • Test fixtures (including test adapters) • Fluid GSE • Miscellanea (MGSE particular items) • Counterbalance Devices (for F/H functional performance testing) • Contamination protection and chemical Cleanliness protection Equipment • Alignment tools

Carrier Module & SCC MGSE (TBC) MGSE typology MGSE item Planetary Protection Req.

Container Transport & Storage Container (Carrier/SCC) N/A Container Solar Array Transport Container N/A Container MGA/HGA Transport Container (if necessary) N/A Handling device Vertical Integration Stand (Carrier/SCC) N/A Handling device Equipment/Panels Integration Trolley & Handling

Set N/A

Handling device Vertical Hoisting Device (Carrier/SCC) N/A Handling device Carrier/SCC Rotating/Tilting Dolly N/A Handling device Horizontal Hoisting Device (Carrier/SCC)

N/A

Handling device Handling Transport Adapter (Carrier/SCC) N/A Test fixture Solar Array Deployment Device N/A Test fixture HGA Deployment Device N/A Test fixture Handling & Test Clamp Band (Carrier/SCC) N/A Fluid (Propulsion) Pressurization Device N/A Fluid (Propulsion) Unit Tester (UPS SCOE) N/A Fluid (Propulsion) Simulant Loading Device N/A Fluid (Propulsion) Propellant Loading Device N/A Fluid (Propulsion) Thruster Leak Test Adapter, with std I/F (e.g. KT N/A

Comment [DBM1]: SCC alcuni applicabili, CM lasciare un TBC per alcune operazioni Aclarar insieme che cosa fa che cosa per definire quando il PP req e’ applicabile

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MGSE typology MGSE item Planetary Protection Req. flange) to leak detectors

Fluid (Propulsion) Dedicated Fluid I/F adapters kit (Ground Half Couplings) with standard interface to FGSE

N/A

Miscellanea Alignment Tool Kit N/A Miscellanea Carrier/SCC Protection Covers N/A ALD MGSE

MGSE tipology MGSE item Planetary Protection Req. Container ALD Transport & Storage Container (ATC) Applicable Handling device ALD Upper Panel Tilting Stand (AUTS) Applicable (in UCZ

ultraclean area) Handling device ALD Lower Panel Tilting Stand (ALTS) Applicable (in UCZ

ultraclean area) Handling device ALD Integration Dolly (AID) Applicable Handling device ALD Panel Assembly Device (APAD) Applicable (in UCZ

ultraclean area) Handling device ALD Hoisting Device (AHD) Applicable Handling device ALD LHP Handling Fixture (ALHF) Applicable Fluid ALD FGSE (TBD) Partially Applicable Miscellanea ALD Alignment Tool Kit (AAK) Applicable (in UCZ

ultraclean area) Miscellanea Protection Covers (TBD) Applicable

Comment [DBM1]: SCC alcuni applicabili, CM lasciare un TBC per alcune operazioni Aclarar insieme che cosa fa che cosa per definire quando il PP req e’ applicabile

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Spacecraft Composite MGSE (TBC) MGSE typology MGSE item Planetary Protection Req.

Test fixture SCC Mass Properties Test Adapter N/A Test fixture SCC Vibration Test Adapter N/A Test fixture SCC Acoustic Test Adapter N/A Miscellanea Access/Working Platform N/A Rover Module MGSE (TBC)

Descent Module MGSE (TBD) Note: All the MGSE in contact with the Rover Module items shall have Planetary Protection more stringent constraints than in the present document.

MGSE typology MGSE item Planetary Protection Req. Container RM Transport & Storage Container Applicable Container RM Solar Array Transport Container Applicable Handling device RM Vertical Integration Stand Applicable Handling device RM Turnover Trolley Applicable Handling device RM Hoisting Device Applicable Handling device Lifting frames + Handling slings Applicable Handling device SA Support Frames Applicable Handling device Drill Handling/Hoisting Device Applicable Test fixture RM Thermal Test Adapter Applicable Test fixture RM Vibration Test Adapter Applicable Test fixture RM Mass Properties Adapter Applicable Test fixture RM Acoustic Test Adapter Applicable Miscellanea RM Protection Covers Applicable Miscellanea RM Temporary Bio-barrier Equipment Applicable Miscellanea Alignment Target/Equipment Jigs Applicable Miscellanea Replacement HDRMs Applicable Miscellanea Mass Dummies Applicable

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5. GENERAL PERFORMANCE REQUIREMENTS

The MGSE design will satisfy the requirements of functionality, safety, transportability that shall be met in the most effective manner. The whole set of the MGSE will be designed to withstand the most sever natural environment conditions, envisaged during its usage in support of the ExoMars space segment/module on ground operations, without detrimental deformation and/or loss of functionality. The design will be carried out to guarantee that the ExoMars space segment/module design will not be subjected to constraints due to MGSE induced loads conditions. MGSE items entering and operating in an ISO 7 HC and inside the ISO 3 clean room shall be designed to comply with PP implementation Planetary Protection Requirements, as defined in chapter 13.0 (see also [IR 05011]), and the Cleanliness & Contamination Control (C & CC) of organic contaminants (particulate and molecular contamination) requirements (see [IR 05014] and [IR 0438]), as applicable .

5.1 Items Standardization

M2-MGSE-REQ-0010 Items Standardization

Verification: [EQP: RoD]

Traces: MGSE shall be designed so that it can be constructed as much as possible by modular/common items and standardized items.

5.2 Interface Design

The MGSE will be compliant to the following interface general design requirements. M2-MGSE-REQ-0020 Installation


Traces: The MGSE to F/H interface design shall avoid incorrect installation of F/H into MGSE itself.

M2-MGSE-REQ-0030 Interface Functional Capability

Verification: [EQP: A, T, RoD]

Traces: The MGSE to F/H interface design shall allow the MGSE of performing its function for all required F/H configurations.

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M2-MGSE-REQ-0040 Unplanned Movements


Traces: The interface design shall be capable of preventing unplanned movements between the MGSE and flight hardware contact surfaces.

M2-MGSE-REQ-0050 I/F Loads

Verification: [EQP: A]

Traces: In case flight interfaces are used, the transmission forces between MGSE/MTSE and F/H interface contact points/areas shall be determined and clearly identified in the relevant analysis report.

M2-MGSE-REQ-0060 Mating/De-mating


Traces: The MGSE to F/H interface design shall provide mating/de-mating with standard tools.

M2-MGSE-REQ-0070 Cleanliness

Verification: [EQP: RoD, I]

Traces: The MGSE interface to F/H shall be designed to be easily cleanable (e.g. with flat surfaces), in order to reach the cleanliness level of the F/H (according to paragraph 11.1.10 of [IR 0112], for Rover Module and ALD MGSE, and paragraph 11.1.7 of [IR 05008] for the MGSE of all other F/H modules) and made of manufacturing materials with no sensitivity to cleaning agents (see Planetary Protection Requirements), to comply with requirements M2-CL-0021 and M2-CL-0022 of [IR 05014] and with [IR 0438].

M2-MGSE-REQ-0080 Clearance


Traces: Clearance between MGSE and F/H dynamic envelopes shall be ≥ 100 mm.

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M2-MGSE-REQ-0090 Special Tools


Traces: Where constraints require special tools for mating of interfaces, the tools shall be identified for use with the particular MGSE and it shall be subjected to the requirements of this specification; any special tool shall be delivered in conjunction with the MGSE.

M2-MGSE-REQ-0100 Adjustment


Traces: The MGSE hardware shall be adjustable (if necessary) to perform the required alignment and correct interfacing of the MGSE itself with F/H.

M2-MGSE-REQ-0110 Assembly Inspection


Traces: Capability shall be provided to inspect assembly and verify the interface integrity of the MGSE sub assemblies that shall be assembled to form the complete item.

M2-MGSE-REQ-0120 Re-assembly Instructions


Traces: MGSE, that may be disassembled and require re-assembly prior to use, shall carry the necessary I/F clear marks and instructions for assembly.

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5.3 Handling/Hoisting

The MGSE will be compliant to the following handling design requirements.

M2-MGSE-REQ-0130 Hand Lifted Max Weight


Traces: All MGSE components heavier than 20 kg shall provide handles for two persons (max weight 33 kg, see req. M2-MGSE-REQ-1620), towing, fork-lift and/or crane interfaces to be moved inside the facilities.

M2-MGSE-REQ-0140 Lifting Point Marking

Verification: [EQP: I]

Traces: Attachment points for hoisting and handling shall be marked or labeled on all equipment as per paragraph 5.11 of this specification.

5.4 Stability

M2-MGSE-REQ-0150 Stability

Verification: [EQP: A, RoD]

Traces: Stability of the MGSE/MTSE, unloaded or loaded by the F/H, shall be verified under any maximum combination of the applicable limit loads; a minimum safety factor of 1.2, equivalent to the ratio between stabilizing and overturning moment, shall be obtained.

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5.5 Parking

M2-MGSE-REQ-0160 Parking


Traces: MGSE shall have adequate provisions to support safe parking positions and guidance.

5.6 Displacements

M2-MGSE-REQ-0170 Displacement Provisions


Traces: MGSE/MTSE items, where applicable in their dedicated specification, shall be provided with swivel castors, lockable and provided with independent brakes, to allow easy displacement inside facilities.

5.7 Life Time

The MGSE will be compliant with the following Life Time design requirements. M2-MGSE-REQ-0180 Useful Life


Traces: AIV Requirement Document #AIV-VER-175

MGSE shall have an operational life of 6 years starting from the delivery of the F/H to the Prime. This requirement allows periodic inspections, preventive maintenance, restoration and components replacements.

M2-MGSE-REQ-0190 Limited Life Item


Traces: The use of Limited Life Items shall be as far as possible avoided.

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M2-MGSE-REQ-0200 Limited Life Item Utilization Exc eption


Traces: If utilization of limited life time cannot be avoided, the MGSE/MTSE design shall enable replacements of such components. Contractor shall require TAS-I approval before utilization of limited life items.

M2-MGSE-REQ-0210 Limited Life Item List


Traces: A limited-life list, included in the MGSE ADP, shall contain:

• the item part number and name • life limit, life limit parameter or part/material and its function • any limitations on number of refurbishment • any restriction related to operational use, test, handling inspection or maintenance.

5.8 Maintainability

The MGSE design will have suitable features such to allow the accomplishment of the here after minimum maintenance requirements, during any ground phase.

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M2-MGSE-REQ-0220 Maintainability


Traces: The MGSE design shall have suitable features such to allow the accomplishment in safe condition of the necessary maintenance requirements, during any ground phase. No numerical reliability assessment shall be performed for the MGSE items. However, judgment and acceptance of these items shall be based on design margins applied, possible failure modes and their effect, and soundness of the design.

M2-MGSE-REQ-0230 Maintenance Unavailability Period


Traces: The period of unavailability for maintenance shall be less than 20 days (including time needed for resetting/readjustments, as applicable).

M2-MGSE-REQ-0240 Failure Unavailability Period


Traces: The period of unavailability in the event of failure shall be less than 30 days (including failure diagnosis, procurement of spares and, as applicable, resetting /readjustments).

M2-MGSE-REQ-0250 Protection for Personnel


Traces: The MGSE shall include protective provisions, if there are potential risks for personnel during maintenance activities.

M2-MGSE-REQ-0260 Replacement


Traces: The MGSE design shall allow easy removal and replacement of all the parts that are subject to deterioration.

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M2-MGSE-REQ-0270 Preventive Maintenance


Traces: The preventive maintenance cycles shall be as specified into the proper procedure provided by MGSE. Adequate self-test facilities (if any) shall be incorporated into the MGSE to minimise the MTTR (Mean Time To Repair).

5.8.1 First Line Maintenance

M2-MGSE-REQ-0280 On-line Maintenance


Traces: On line MGSE maintenance philosophy shall be based, as primary mode, on corrective instrument/unit removal and replacement to minimise the non-availability of the MGSE to support AIT operations and to minimise support costs.

M2-MGSE-REQ-0290 Off-line Repair


Traces: Repairs of replaced items shall be performed off-line.

5.8.2 Spare Parts

To establish and identify spares for ExoMars Spacecraft MGSE the following phylosophy is applied. M2-MGSE-REQ-0300 Spare Number


Traces: The MGSE shall be designed to use common hardware and standard parts, to reduce the number of spare types (if any) and repair parts required for support.

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M2-MGSE-REQ-0310 Consumable Spare


Traces: All the MGSE shall be provided with a minimum of 10% of spare consumable items to comply with the requirements of unavailability time identified in M2-MGSE-REQ-0230 and M2-MGSE-REQ-0240.

M2-MGSE-REQ-0320 Spare Tool


Traces: In case special (not commercial) tools will be manufactured for assembly, maintenance and/or use of the MGSE, at least one spare for each tool shall be provided.

5.8.3 Accessibility

M2-MGSE-REQ-0330 Accessibility


Traces: Provisions shall be made for the removal and replacement of all parts subjected to wear, deterioration or change. MGSE design shall permit access to interior parts for easy removal of major components part.

M2-MGSE-REQ-0340 Replaceable Component


Traces: Components subject to normal replacement or servicing shall not be secured by rivets, welding or other means that would prohibit easy removal.

5.8.4 Standardization

Standardization will be incorporated in the MGSE for its hardware, technical data formats, format access and procedures to facilitate maintenance.

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M2-MGSE-REQ-0350 Standardization Tools and Fixture s


Traces: The MGSE shall be designed to provide maximum compatibility for use with commercial metric standard tools.

M2-MGSE-REQ-0360 Torque and Special Tools


Traces: Torque values and recommended special tools for all threaded fasteners and fittings shall be specified in the design reports and on drawings.

5.9 Transportability

MGSE design will comply with the following requirements. M2-MGSE-REQ-0370 Transportation Provisions


Traces: Packed equipment and shipping containers shall incorporate lifting provisions for loading/unloading and tie-down provisions for avoiding displacements during transportation.

M2-MGSE-REQ-0380 Dimension Constraints


Traces: Maximum container dimensions shall be compatible with the international standard constraints of air, road, sea and rail transportation modes (see para 6.3). As far as not specified otherwise herein, MGSE design shall meet the requirements contained in document [RD A111].

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5.10 Nameplates and Product Marking

MGSE design will comply with the following requirements. M2-MGSE-REQ-0390 Part Numbering


Traces: Each MGSE part shall be uniquely identified by its Part-Number. Part Number is an identification number assigned by the Design Authority to the part and it is clearly correlated to the manufacturing drawing which defines the item.

M2-MGSE-REQ-0400 MGSE Identification


Traces: All MGSE shall be univocally and permanently identified. Part number shall consist of the contract number followed by unique identifier.

M2-MGSE-REQ-0410 MGSE Labeling


Traces: MGSE shall be permanently marked at least with the following information on dedicated labels:

• Project name • Item name • Manufacturer's name or code • Manufacturer's Identification number • Configuration Item number • Part number • Serial number • Mass [Kg]

All items subjected to periodic proof load shall have proof-load tag containing the proof load and the next proof test due date.

M2-MGSE-REQ-0420 Marking Lifetime


Traces: Markings shall remain legible for the operational life of the item it is affixed to.

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M2-MGSE-REQ-0430 Marking Techniques


Traces: Marking techniques shall not degrade the structural integrity of the item.

M2-MGSE-REQ-0440 Hoisting Points Identification


Traces: All hoisting points and tie-down points shall be clearly marked or labelled.

M2-MGSE-REQ-0450 Control of Lifting MGSE Re-Assemb ly


Traces: All lifting/hoisting components which are normally disassembled such as individual slings, cables, shackles, pins and similar parts shall tether serialized, tagged or marked for positive identification to assure proper re-assembly.

5.11 Workmanship

M2-MGSE-REQ-0460 Workmanship


Traces: The MGSE shall be designed, fabricated and finished for high quality of fit and finish and for adherence to specified dimensions and tolerances requirements. In case of deviations, the normal non-conformance control procedure shall be applied. Quality Assurance shall control through planned inspection points fabrication operations, including assembling and testing, in order to ensure that the design criteria specified is achieved. Non destructive testing methods (NDI), such as dye penetrant inspection and other applicable methods shall be used to ensure that the hardware is of high quality.

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6. INTERFACE REQUIREMENTS

The MGSE I/F general requirement description is here in the following given.

6.1 MGSE to F/H Interfaces

M2-MGSE-REQ-0470 I/F to Flight Hardware


Traces: AIV Requirement Document #AIV-VER-290 All ALD MGSE I/F shall be compatible with the F/H interfaces as per [IR 0424] and [IR 0443]. F/H I/F of other MGSE under TAS-I procurement responsibility are currently TBD.

M2-MGSE-REQ-0480 I/F Contact Material


Traces: MGSE parts interfacing with F/H shall be provided with adequate protection provisions (e.g. coated by softer material) or be configured to preclude damage to the F/H surfaces by normal and improper handling during attachment/removal/utilization procedures, according to paragraph 11.1.9 of [IR 0112] for Rover Module and ALD MGSE and paragraph 11.1.6 of [IR 05008] for MGSE of all other F/H modules.

6.2 MGSE to Facilities Interfaces

M2-MGSE-REQ-0490 I/F to Facilities


Traces: AIV Requirement Document #AIV-VER-300 All I/F of MGSE used at integration, test and launch site shall be compatible with all the facilities, including launch site, in terms of:

• Doors dimensions, crane height from floor, crane hook dimensions • Uniformly distributed and concentrated allowable load on floor • Power, air and GN2 supply • Electrical Grounding point

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M2-MGSE-REQ-0500 I/F to Integration Facilities


Traces: MGSE shall be compatible with following integration facilities characteristics. TAS-I, ISO 7 HC and ISO 3 facilities TBD ASTRIUM UK facility: TBD Launch facility: TBD

M2-MGSE-REQ-0510 I/F to Test Facilities


Traces: MGSE shall be compatible with TBD Test Facilities.

M2-MGSE-REQ-0520 Electrical Power Supply I/F


Traces: In case the MGSE will be provided with electrical devices, the electrical power circuits shall be designed to interface with the following power supply: TAS-I and European Integration and Test Facilities - single phase: 220 V ± 10% ; 50 Hz ± 1Hz - three phase: 380 V ± 10% ; 50 Hz ± 1Hz Launch, Processing and Fueling Facilities TBD

REFERENCE : DATE :


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M2-MGSE-REQ-0530 GN2 Connection I/F


Traces: The GN2 standard bottles and racks, for F/H container purging system, have Italian, German, Dutch, French or English I/F. In case a container will be provided with an installation for a GN2 supply, a set of adapters for the various above I/F’s shall be provided as items of the MGSE (not as quick disconnect because of the high pressure involved of 200 bar).

M2-MGSE-REQ-0540 I/F to EDU


Traces: MGSE alone or carrying F/H weighing more than 1500 kg shall provide adequate I/F to the EDU, in accordance with the following Fig 6.2-1 (TBC).

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Figure 6.2-1: I/F to EDU

M2-MGSE-REQ-0550 Wheels Provisions


Traces: All MGSE required to be moved within facilities on wheels or parked on supporting pads shall respect the requirement of maximum concentrated load on floor as per M2-MGSE-REQ-0500 and M2-MGSE-REQ-0510.

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6.3 MGSE to Transportation Means Interfaces

M2-MGSE-REQ-0560 Container to Transportation Means I/F


Traces: F/H Transport & Storage Container and MGSE shipping container/boxes shall respect requirements for compatibility with transport vehicles such as trucks, barges, ships and aircraft and with the associated handling equipment or facilities.

M2-MGSE-REQ-0570 Compliance to Transportation Stan dard Rules


Traces: The MGSE packaging shall conform to the European and American Standard Rules for road, air and ship transportation and shall also consider facility and road constraints (e.g. bridges, tunnel).

M2-MGSE-REQ-0580 I/F to Standard Transportation Me ans


Traces: All transport containers shall be designed for road, air and ship transportation by standard commercial means readily available in Europe, as applicable (except for F/H Transport & Storage Container and containers for MGSE of large dimensions).

M2-MGSE-REQ-0590 I/F to Road Transport


Traces: The shipping containers/boxes of the MGSE (except those for MGSE of large dimensions) shall meet international standards for road transport to minimize special handling and transport equipment. The relevant height and width limit dimensions of the containers are: 4.0 m (from the ground) x 2.5 m

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MS-MGSE-REQ-0600 I/F to Air Transport


Traces: The IATA regulations, as per [RD 09], shall apply. Particularly for emergency case, decompression safety device (burst disk, burst flap) shall be installed on the containers in accordance to the international IATA flight regulations, as defined in [RD 09]. F/H Transport Container and MGSE shipping boxes shall be compatible with the Cargo Bay of the cargo aircraft selected for transport to launch facility. The MGSE Transport Containers shall be then compatible with relevant “Cargo Aircraft User Manual”. The following figure shows the dimensions of a possible cargo aircraft, e.g. Antonov AN-124:

Figure 6.3-1 : Cargo Bay Dimensions of Antonov AN-124

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7. DESIGN AND CONSTRUCTION REQUIREMENTS

7.1 General Design Requirements

The MGSE will be designed, fabricated and finished to a high quality of fit and finish and for adherence to the specified requirements. M2-MGSE-REQ-0610 International System Measurement Unit


Traces: The “International System of Units” shall be applied for MGSE design.

M2-MGSE-REQ-0620 Coordinate System & Reference Mar ks


Traces: The MGSE in general shall use the Reference Axis System of the interfaced F/H. For the ALD MGSE the Reference System shall be that defined in the [IR 0424]. All MGSE (adapter, trolley, stand, and lifting devices) interfacing to F/H shall clearly show the co-ordinate system and shall have engraved reference marks (at upper and lower I/F flange) where F/H is mounted.

M2-MGSE-REQ-0630 Design Normative


Traces: The MGSE shall be designed in accordance with the European Standard e.g. ISO, DIN.

7.2 Mechanical Design

M2-MGSE-REQ-0640 MGSE Weight and Size


Traces: The design of the MGSE shall generally minimise weight and size to avoid any excess not required by equipment functionality.

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M2-MGSE-REQ-0650 Load Environment


Traces: Load environment experienced by MGSE structure (when loaded or not by the F/H) and by the MGSE to F/H interfaces shall be that defined in paragraphs 8.4.1 and 8.4.2.

M2-MGSE-REQ-0660 Safety Factors & Margin of Safety

Verification: [EQP: A, T, RoD]

Traces: The safety factors to be used for the MGSE design are here after defined: - TRANSPORT CONTAINERS, ADAPTERS, CLAMP BANDS, SUPPORT STANDS & WORKSTANDS

• Yield Safety Factor : FOSY = 3 • Ultimate Safety Factor : FOSU = 4 • Proof Factor : FOSP = 1.5

- LIFTING/HOISTING DEVICES & ACCESSORIES • Yield Safety Factor : FOSY = 3 • Ultimate Safety Factor : FOSU = 5 • Proof Factor : FOSP = 2.0

NOTE: It is worth to clarify that, regarding the Lifting Devices or Slings, the proof mass (or mass dummy) used for relevant proof load shall be representative of twice the mass of the lifted assembly (e.g. for the Lifting Device of the Transport Container the proof mass shall be two times the total mass of the Transport Container plus loaded F/H) The stress analysis shall be performed in order to verify the mechanical integrity of all main structural components by calculating positive margins of safety according to following relation: MOS = Yield or Ultimate Strength / (Design Limit Load x Yield or Ultimate Safety Factor) – 1 > 0 Following table summarizes design and proof safety factors for all MGSE items:

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Table 7-1 : MGSE Design and Proof Safety Factors

GROUND SUPPORT EQUIPMENT YIELD

FOSY ULTIMATE

FOSU PROOF 1), 2), 3)

FOSP

REFERENCE

SLINGS: Wire Rope 3.0 5.0 2.0 DIN EN 13414-1 Alloy Steel Chain 3.0 5.0 2.0 DIN EN 818-4 Metal Smash 3.0 5.0 2.0 DIN EN 13411-3 NATURAL & SYNTHETIC ROPE: Polypropylene - 7.0 2.0 DIN EN 1492-2 Polyester - 7.0 2.0 DIN EN 1492-2 Nylon - 7.0 2.0 DIN EN 1492-2 MGSE ITEM: Lifting Devices:Eye Bolts, Eyelets, Pins, Shackles, Links, Rings and Spreader Beams

3.0 5.0 2.0 DIN EN 13889

Transport Container 3.0 4.0 1.5 / Load Cells for Weight/Balance 3.0 5.0 2.0 VDI/VDE 2637 Hydrasets 3.0 5.0 2.0 NSS/GO-

1740.9B Adapters, Clamp Bands & Support Stands

3.0 4.0 1.5 DIN 5081

Work Stands 3.0 4.0 1.5 VFN 58501 PRESSURIZED MGSE: Verification w.r.t. max. working pressure

Pressurised Flex Hoses 2.0 4.0 1.5 ISO 4413 ISO 4414

GSE Pressurised Components 2.0 4.0 1.5 ISO 4413 ISO 4414

GSE Pressure Vessel, hydrostatical GSE Pressure Vessel, pneumatical

2.0 2.0

4.0 4.0

1.5 1.5

ISO 4413 ISO 4414

COMMERCIAL ITEMS: Wheel Supports, Swivel Castors Screw-jacks, gear boxes, bearings, etc…

/

*

1.5

/

NOTE: 1) All the MGSE annually proof loaded shall have "proof load tags", "proof load date" and QC stamps 2) Annual re-certification according to national and launcher site regulation 3) For Transport Containers the proof factor 1.5 is only used for static proof load of the main structural parts (e.g. the cradle, base frame, etc..), while for the lifting points a proof factor of 2 shall be applied * The design load D.L. of generic commercial item shall be calculated as: D.L. = L.L x FOS , with L.L. = limit load on most stressed item, obtained by static analysis of the MGSE based on application of the load factors defined in Table 8-1 of M2-MGSE-REQ-1400, and FOS = safety factor = 1.5

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7.2.1 Attenuation System Requirements

The attenuation system of the F/H Transport Containers will be compliant with the following dynamic requirements. M2-MGSE-REQ-0670 De-coupling Requirements


Traces: AIV Requirement Document #AIV-VER-280 The eigen-frequency values of the attenuated system (F/H plus damping system) shall be such that potential dynamic coupling with the F/H fundamental frequencies and from the truck suspension system are avoided.

M2-MGSE-REQ-0680 Design Criteria


Traces: A resultant transport environment obtained by the combination of the sinusoidal and random vibrations defined in paragraph 8.4.2 shall be considered for the attenuation system design. Such vibration environment shall be determined starting from the assumptions and the method of combining the input vibrations as defined here in the following.

M2-MGSE-REQ-0690 Random Acceleration Amplitude


Traces: An approximate normal (Gaussian) distribution shall be assumed and a 3σ instantaneous amplitude shall be used for determining the maximum contribute of the random accelerations.

M2-MGSE-REQ-0700 Vibration Combination Method


Traces: The recommended method for combining sinusoidal and random acceleration shall be as follows: for each axis the random acceleration peak response is to be added to the corresponding sinusoidal acceleration response (considered as a dwell input at any frequency). The resulting sum in that axis has to be combined with the sinusoidal response in two remaining orthogonal axes.

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This results in a set of three quasi-static load cases, here after illustrated by the Table 7-2, to be considered verifying that they are not exceeding the maximum quasi-static accelerations (load factors) defined in paragraph 8.4.1.

Table 7-2 : Sinusoidal and Random Acceleration Combination Method

Load Set x-axis y-axis z-axis

1 ± (Sx+Rx) ± Sy ± Sz 2 ± Sx ± (Sy+Ry) ± Sz 3 ± Sx ± Sy ± (Sz+Rz)

NOTE: 1) S = sinusoidal response (100% along z-axis and 66% along x and y-axis); R = random response • Loads in each axis acting simultaneously • Contribute of 1 [g’s] due to gravity (assumed positive in down direction) shall be also added to the resultant accelerations along z-axis 4) The acceleration measurement unit is the gravity To evaluate the random acceleration response at F/H due to a random input (for single degree of freedom system only), the following Miles’s relationship has to be used: Ri = 3ν (π/2 ∗ fn,i ∗ T ∗ Wf,i) , where: i = x, y, z axis index Ri = induced random acceleration [g’s] fn,i = attenuated system (damped frame plus F/H) natural frequency [Hz] Wf,i = power spectral density [g2/Hz] T = transmissibility at resonance of the selected shock absorber To evaluate the sinusoidal acceleration response the following relationship has to be used: Si = T ∗ gsi ∗ αi , where: gsi = peak acceleration obtained from the sinusoidal input of paragraph 8.4.2, versus the attenuated system natural frequency αi = percentage value (of sinusoidal peak acceleration) as a function of the axis direction (αx = 66 % ; αy = 66 % ; αz = 100 % )

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M2-MGSE-REQ-0710 Transport Shock Response


Traces: AIV Requirement Document #AIV-VER-280 Resultant accelerations at F/H CoG, in response to shock impulse of req. M2-MGSE-REQ-1430, shall not exceed the maximum quasi-static accelerations allowed on transported F/H defined in paragraph 8.4.1.

M2-MGSE-REQ-0720 Drop Shock Response

Verification: [EQP: A, T]

Traces: Resultant accelerations, obtained in response to a drop of the F/H Transport Container as per req. M2-MGSE-REQ-1440, shall not exceed the 80% of the F/H maximum design load factors (TBD for ALD)

7.3 Parts, Materials and Processes

7.3.1 Materials

M2-MGSE-REQ-0730 Manufacturing Material General Re quirements


Traces: AIV Requirement Document #AIV-VER-310 The manufacturing materials of the MGSE items shall consider the cleanliness level required for ISO 8, ISO 7 HC and ISO 3/ISO AMC-9 clean rooms, as applicable.

M2-MGSE-REQ-0740 Commercial Material


Traces: MGSE manufacturing materials shall be selected considering as much as possible commercial construction products and standard items specified by European normative such as DIN, BS, UNI, ISO, etc..

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M2-MGSE-REQ-0750 Structural Metallic Material


Traces: Following metallic materials can be used in general for the MGSE manufacturing: • low carbon steel or steel alloy, corrosion protected by adequate surface treatment resistant to IPA wiping • stainless steel • titanium (not applicable for connection hardware items) • aluminium or aluminium alloy, corrosion protected by adequate surface treatment resistant to IPA wiping • bronze, brass and copper alloy (for bush, threaded bars, female nuts, sliding pads, pins, etc..) For the manufacturing of the ALD MGSE operating in ISO 3/ISO AMC-9 low carbon steel and steel alloy metallic material shall be avoided.

M2-MGSE-REQ-0760 Connection Hardware Material


Traces: For the standard and manufactured connection hardware and fastener components, use of stainless steel material shall be made as much as possible.

M2-MGSE-REQ-0770 Non Metallic Material


Traces: Elastomer and plastic materials shall be avoided to the maximum extent possible, as well as commercial lubrication products (e.g. oil, grease) unless their containment is guaranteed by adequate sealing provisions. In general, use of Teflon and nylon material is allowed, as well as Teflon and dry lubricants. Ceramic materials can be also considered. In particular for the manufacturing of the ALD MGSE operating in ISO 3/ISO AMC-9 use of polymeric and PTFE material shall be avoided.

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M2-MGSE-REQ-0780 Material Restrictions


Traces: Following materials shall not be used for MGSE design: • Beryllium and beryllium alloy • Dichlorethane • Clhlorinated Fluorocarbon • Ethylene Glycol • Mercury

M2-MGSE-REQ-0790 Shatterable Material


Traces: The use of shatterable or flaking materials shall be avoided to the maximum extent possible. Structural equipment materials or surface finishes shall not be susceptible to flaking or otherwise generate particles that would degrade F/H cleanliness level, according to paragraph 11.1.9 of [IR 0112] for Rover Module and ALD MGSE and paragraph 11.1.6 of [IR 05008] for MGSE of all other F/H modules.

M2-MGSE-REQ-0800 Flammability Requirements


Traces: Usage of non-flammable or self-extinguishing material shall be maximised as much as possible (see [RD A106]).

M2-MGSE-REQ-0810 Fungus Resistance


Traces: Used materials shall be fungus resistant or shall be treated to resist fungi.

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M2-MGSE-REQ-0820 Corrosion


Traces: Materials used for the MGSE shall be selected taking into account adequate resistance to corrosion and proper surface treatments, according to paragraph 11.1.9 of [IR 0112] for Rover Module and ALD MGSE and paragraph 11.1.6 of [IR 05008] for MGSE of all other F/H modules. These characteristics shall be assessed according to recognised European standards. This requirement shall be strictly applicable to: - Main load path structural items - Structural parts material without surface protection coating - Item that has I/F with the F/H - Bolts and Fasteners

M2-MGSE-REQ-0830 Dissimilar Metal Assembly


Traces: In case dissimilar metals have to be directly interfaced they shall not generate galvanic couples greater than 0.25 V for MGSE operating in a non-clean environment, or greater than 0.5 V for MGSE operating in a clean-room environment, as specified in following Table 7-3. Optionally, suitable surface protections shall be applied or a material compatible with them shall be interposed to avoid any galvanic corrosion problem.

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Table 7-3 : Compatible Galvanic Couples

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7.3.2 Processes

M2-MGSE-REQ-0840 Material Non Destructive Inspecti on (NDI)


Traces: When MGSE materials are subjected to NDI, a dedicated NDI report shall be prepared and retained by the contractor and released to Customer together with the MGSE hardware itself. Such report shall include as a minimum: • Criteria previously established for the selection of fracture control critical structural areas to be inspected by NDI methods • Criteria used for selection of NDI techniques for fracture control critical components • Measure/Inspection result

M2-MGSE-REQ-0850 Critical Welds


Traces: Critical welds shall be avoided wherever possible. A critical weld shall be defined as a weld, the single failure of which, during any operating condition, could result in the injury to personnel or damage to property or flight hardware. Critical welds shall be analyzed and verified by fail safe/safe life criteria. Appropriate non-destructive testing (NDI) that look inside the weld (such as radiograph and ultrasonic) shall be used for critical weld, if any, in addition to surface methods (such as dye penetrant, magnetic particle, visual inspection).

M2-MGSE-REQ-0860 Critical Weld Identification


Traces: Critical welds shall be identified through design drawings by placing a flag note in the tail of the critical weld symbol. The dedicated appropriate non-destructive testing shall be also identified and reported by general notes in the same design drawings.

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M2-MGSE-REQ-0870 Protective Coatings and Finishes


Traces: The protective coating and finishes for the MGSE components operating inside the ISO 7 HC and ISO 8 HC environments shall be compliant with Planetary Protection Requirements. In general the used coating processes shall be as specified in the following: • critical welds requiring periodic non-destructive testing shall be corrosion protected by a coating of strippable paint, including an area 10÷12 mm wide on each side of the weld bead. • aluminum and aluminum alloy parts shall be protected by surface treatments of chemical oxidation (yellow chromate coating) or anodic oxidation (DC-chromic acid method) • cadmium plating shall not be used • steel alloy not commercial off-the-shelf machined components shall be finished by nickel or chromium plating • steel alloy commercial off-the-shelf standard components, such as screws, nuts, quick fasteners, lifting accessories, etc., shall be protected by zinc dichromate (yellow zinc) plating or by nickel or chromium plating Steel alloys powdered coatings shall be used. Not epoxy paints have to be used. • after nickel or chromium plating treatment of the steel alloy components, a dehydrogenation process shall be performed • commercial off-the-shelf standard components made of corrosion resistant steel shall be preferred as much as possible • exterior metal surfaces, seams and edges coated with an approved epoxy or polyurethane varnish shall not require additional sealing • all MGSE component metal surfaces in contact with F/H having a greater roughness and hardness shall be protected by galvanic coating or softer material compatible with the PPR requirements. Protective coating and finishing of metallic materials used for manufacturing of the ALD MGSE operating in ISO 3/ISO AMC-9 shall be avoided.

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7.4 Electrical Design

The electrical design of the MGSE will be compliant to the here in the following specified requirements. M2-MGSE-REQ-0880 Electrical Design General Require ments


Traces: The MGSE shall avoid any damage to both F/H equipment and MGSE or alteration of the equipment characteristics due to input power malfunction. Grounding and bonding provisions shall be implemented on the MGSE in order to discharge the electrostatic current and fault current due to supported F/H electrical equipment.

M2-MGSE-REQ-0890 Power Supply


Traces: The MGSE electrical power circuit shall be designed for use at integration, test, and launch facilities as per req. M2-MGSE-REQ-0520.

M2-MGSE-REQ-0900 Receptacles and Plugs


Traces: For use at European integration and test facilities the electrical power receptacles and plugs type shall be: 400V IEC 309 CEE 16 A or 32 A ; 230 CEE 16 A. For use at launch and processing facilities the electrical power receptacles and plugs types shall be: TBD

7.4.1 Electrical and Electronic Safety Criteria

M2-MGSE-REQ-0910 Electrical & Electronic Safety No rmative


Traces: All MGSE shall meet the requirements of the appropriate National or International Electric and Fire codes or equivalent European standards and directives as per [RD 01] and [RD 07], according to paragraphs 11.1.11.1 and 11.1.7 of [IR 0112], for Rover Module and ALD MGSE, and paragraphs 11.1.8.1 and 11.1.4 of [IR 05008] for MGSE of all other F/H modules. Moreover the MGSE shall meet the launch site safety rules as per requirements contained in the RD 12] and [RD 13].

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M2-MGSE-REQ-0920 Electrical Safety Protections


Traces: Electrical equipment shall be designed to provide personnel protection from accidental contact with alternating current (AC) voltages in excess of 30 volts root mean square (rms) or 30 volts direct current (DC) or any lower voltage that could cause injury.

M2-MGSE-REQ-0930 Operating Voltage Indication


Traces: All racks, chassis and compartments which contain exposed terminals and similar components shall be clearly marked or labelled to indicate the highest potential present operating voltage, when this exceeds 28V.

M2-MGSE-REQ-0940 “Explosion Proofed” Requirement


Traces: Electrical equipment which is operated during system pressurisation and/or flow of flammable atmosphere (e.g. propellants) shall be "explosion proofed" in accordance with an appropriate European National Standard. Hazard proofing may be obtained by potting, hermetically sealing, or by positive pressurisation with an inert gas or clean air.

M2-MGSE-REQ-0950 Electrical Equipment Control Safe ty Provisions


Traces: Electrical equipment to be operated in enclosed rooms or areas where flammable atmosphere (e.g. propellants) are present but in a static state (i.e. no flow or change of pressurisation), shall be controlled by a switch at a single monitoring station capable of deactivating all non-explosion/"hazard proof" equipment within the area. This station must be manned at all times when the equipment is in use. The master switch shall be explosion/hazard proof if it is located within the hazard area. Equipment which cannot be connected to the master switch shall be identified to the ESA/CNES (LSSO) during the phased safety review process.

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M2-MGSE-REQ-0960 Electrical Contact Resistance

Verification: [EQP: T, RoD]

Traces: All MGSE internal metallic contacts shall provide an ohm resistance of less than 50 mOhm

M2-MGSE-REQ-0970 Electromagnetic Compatibility


Traces: MGSE electrical circuits shall be designed to meet the EMC requirements as per [RD 06] and [RD 13], according to paragraph 11.1.11.1 of [IR 0112] for Rover Module and ALD MGSE and paragraph 11.1.8.1 of [IR 05008] for GSE of all other F/H modules. MGSE with direct F/H interface shall be non-magnetic. Electrical circuits shall not be a source of interference such that spacecraft on-board system performance can be degraded. NOTE: Electromagnetic perturbations fall into two categories: conducted and radiated.

M2-MGSE-REQ-0980 Electrical Motor


Traces: Electrical motors used per MGSE operating in European facilities shall be compliant to the International and European standards.

M2-MGSE-REQ-0990 Electrical Motor Insulation


Traces: Electrical motors shall be isolated from the structure elements.

M2-MGSE-REQ-1000 F/H Insulation from Crane


Traces: Each lifting device shall be equipped with webbing slings so that the F/H to be lifted is electrically isolated from the crane.

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M2-MGSE-REQ-1010 Power Loss Safety Device


Traces: All equipment shall automatically revert to a safe configuration when an input power loss occurs and shall include features that prevent hazardous situations occurring to flight hardware and personnel.

M2-MGSE-REQ-1020 Power-Kill Safety Switch


Traces: GSE shall be provided with a power-kill switch accommodated in accessible places to allow rapid power kill in case of contingencies.

7.4.2 Grounding and Bonding Safety Criteria

M2-MGSE-REQ-1030 Grounding Point Provisions


Traces: The MGSE shall have at least two grounding points (studs or straps as applicable), one for connection to the facility grounding net and one for connection to the flight hardware or other MGSE item. The possibility of grounding of every metallic part of equipment shall exist. MGSE Grounding system shall be designed according to appropriate national/international standards and launch site safety rules.

M2-MGSE-REQ-1040 Grounding Connections


Traces: Grounding/bonding connections shall be designed to minimise the possibility of inadvertent disconnection, e.g.: • solder shall not be used for external connections • threaded fasteners shall use lock washers

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M2-MGSE-REQ-1050 Bonding Straps & Jumpers


Traces: GSE bonding straps and jumpers shall be copper and shall have a cross-sectional area of not less than that of a No. 6 AWG copper wire.

M2-MGSE-REQ-1060 Grounding Characteristic for EMC


Traces: MGSE shall provide grounding to F/H compatible with EMC requirements (e.g earth loop shall be avoided).

M2-MGSE-REQ-1070 Mobile Equipment Grounding Provis ions


Traces: All mobile or portable equipment shall have static ground provisions.

M2-MGSE-REQ-1080 MGSE Grounding Resistance Feature s

Verification: [EQP: T, RoD]

Traces: All trollies, adapters and stands shall be provided with electrical grounding points to facilitate connection to the local grounding system. The resistance measured between the interface of the item and the ground point shall be less than 100 mOhm (under 1A). Bonding point: M8

M2-MGSE-REQ-1090 Grounding Cable Length


Traces: A green-yellow cable having minimum length of 15 m shall be provided in order to perform MGSE to facility grounding point connection.

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M2-MGSE-REQ-1100 Electrical Resistance from MGSE t o Facility Grounding

Verification: [EQP: T]

Traces: The DC electrical resistance between the MGSE and facility grounding point shall not exceed 10 Ohm.

7.4.3 Cable and Wiring Safety Criteria

M2-MGSE-REQ-1110 Cable and Connector Installation Features


Traces: All electrical connections and cable installations shall be designed with sufficient flexibility, length and accessibility to permit disconnection and reconnection without damage to wiring or connectors.

M2-MGSE-REQ-1120 Solid Wire


Traces: Solid wire (single strand) shall not be used in locations where it may be subjected to flexing.

M2-MGSE-REQ-1130 Cable and Wire Marking


Traces: All electrical cables and wires shall be marked to clearly indicate the correct mating connection or termination point to preclude phase reversal or cross-connection.

M2-MGSE-REQ-1140 Cable and Wire Clamping


Traces: All electrical cables and wiring shall be clamped and supported to remain clear of sharp edges and moving parts and to eliminate mechanical stress on wires, terminations and connectors.

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M2-MGSE-REQ-1150 Wires Insulation


Traces: Dead end wires shall be completely insulated.

M2-MGSE-REQ-1160 Cable Protection


Traces: Cables extending across work areas shall be protected.

7.4.4 Connector and Switch Safety Criteria

M2-MGSE-REQ-1170 Power Connector


Traces: Only female connectors shall be used as sources of power.

M2-MGSE-REQ-1180 Switch Marking


Traces: All switches shall be clearly marked or labelled to indicate the system function for each switch position.

M2-MGSE-REQ-1190 Electrical Component Safety Desig n Precautions


Traces: All mating items (fluid, mechanical, electrical and optical connectors, plugs, or similar) shall be designed to make it physically impossible to inadvertently reverse a connection or mate the wrong connectors if a hazardous condition can be created.

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7.4.5 Overload Protection

M2-MGSE-REQ-1200 Visual Provisions


Traces: Circuit breakers shall provide a visual indication when tripped.

M2-MGSE-REQ-1210 Electrical Parameters Indication


Traces: Electrical fuse and switch boxes shall be stencilled on the outside or inside cover to show the voltage present, rated fuse capacity, and equipment that the circuit controls.

M2-MGSE-REQ-1220 Overload Protection Provisions


Traces: Malfunction of the spacecraft or MGSE circuitry shall not induce overload into the launch/servicing vehicle, MGSE or facilities.

M2-MGSE-REQ-1230 Circuit Breakers Trip Provisions


Traces: Circuit breakers shall trip and protect the circuit even if the switch lever is physically held in the "ON" position.

M2-MGSE-REQ-1240 Overload Protection Installation


Traces: Overload protection devices shall be installed in each ungrounded conductor in three (3) phase power systems and shall be designed so that all three (3) devices trip simultaneously.

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M2-MGSE-REQ-1250 Circuit Breaker Setting Indicatio n


Traces: All adjustable type circuit breaker settings shall be specified in the design.

M2-MGSE-REQ-1260 Circuit Breakers Sizing


Traces: All circuit breakers shall be sized (or set) to protect the smallest wire within a circuit, including all branches, which do not have independent circuit protection.

M2-MGSE-REQ-1270 Overload Protection Device Sizing


Traces: Overload protection devices shall be sized (or set) so that the combination of current and time at which the device operates will not cause the operation of upstream protective devices.

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8. ENVIRONMENTAL REQUIREMENT

The MGSE will be designed to withstand the most severe natural environment that may be encountered during the operative/not operative conditions, without impairment of its performances for any time period compatible with their useful life. The environment experienced by the MGSE is relevant to: • Integration, test and launch site facilities • Open or sheltered area during not operative storage • Road and air transport

8.1 Integration and Test Facility Environment

In general the MGSE will be designed to operate into clean room areas ISO 7 HC and ISO 8. Particularly for the integration of the ALD, some MGSE shall be designed to operate inside an ISO 3 AMC-9 ultra-clean area typical of Glove Flowbox Isolators. The here below environmental parameters shall be considered. M2-MGSE-REQ-1280 Temperature


Traces: The MGSE shall be designed to operate at a temperature of 22 ± 3 ºC.

M2-MGSE-REQ-1290 Humidity


Traces: The MGSE shall be designed to operate at humidity levels ranging from 45 % to 65 % RH, at a temperature range of 22 ± 3 ºC.

M2-MGSE-REQ-1300 Pressure


Traces: Concerning the ISO 7 HC and ISO 8 clean rooms the pressure shall be the ambient one, i.e. from 0.85 to 1.04 bar. For the ISO 3 AMC-9 ultra-clean area an overpressure of 0.5 mbar w.r.t. the ambient one shall be considered.

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MS-MGSE-REQ-1310 Facilities Environment Cleanlines s


Traces: The MGSE cleanliness level shall be compatible with the integration and test facilities cleanliness class inside it is operating, i.e. with the one of:

• ISO 8 HC clean room • Bioburden strictly controlled ISO 7 HC clean room • ISO 3 AMC-9 ultra-clean area

8.2 Storage in External Environment

The following requirements are applicable to the Transport Containers of F/H and to the shipping containers stowing the MGSE, when stored in open air. M2-MGSE-REQ-1320 Temperature


Traces: The MGSE shall be designed to operate in a range of temperature from −40 to +60 ºC.



Traces: The MGSE shall be designed to operate at a Relative Humidity ≤100%.



Traces: The considered pressure shall be the ambient one, i.e. from 0.85 to 1.04 bar.

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M2-MGSE-REQ-1350 Outdoor Environment Cleanliness


Traces: An uncontrolled cleanliness environment shall be considered.

8.3 Transport Environment

The following requirements are applicable to the Transport Containers of F/H and to the shipping containers stowing the MGSE during transportation phases. M2-MGSE-REQ-1360 Temperature


Traces: The MGSE shall be designed to operate in a range of temperature from −40 to +60 ºC (TBC).



Traces: The MGSE shall be designed to operate at a Relative Humidity ≤100%.



Traces: The considered pressure shall be as follows:

• during road transport it shall be the ambient one, i.e. from 0.85 to 1.04 bar. • during air transport in not pressurized cargo, the considered pressure shall be in a range from 1050 hPa to that equivalent to 15 km of altitude

The following rate of pressure change during air transportation (air freighting condition) shall be also considered:

• during ascent a decrease of 143 Pa/sec • during descent an increase of 143 Pa/sec

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M2-MGSE-REQ-1390 Transport Environment Cleanliness


Traces: An uncontrolled cleanliness environment shall be considered.

8.4 On-Ground Mechanical Environment

The mechanical environment experienced from the MGSE during integration, handling and transportation is herein described.

8.4.1 Design Load Factors

The limits load factors reported in the following paragraphs are applicable to MGSE design. M2-MGSE-REQ-1400 Load Factors (or Quasi-static Acc elerations)


Traces: The MGSE shall be designed considering the load factors defined in following table:

Table 8-1 : MGSE Quasistatic Load Factors

Operation Direction of Applied Force Load Factor Hoisting Vertical -1.3 g Hoisting and lateral motion

Vertical +Horizontal (simultaneously)

-1.3 g ± 0.2 g

On integration dolly (slow displacements inside facilities)

Vertical +Horizontal (simultaneously)

-1.1 g ± 0.2 g

Tilting on integration dolly In the tilting plane -1± 0.2 g Transportation Vertical

+Horizontal in main moving direction +Horizontal perpendicular to main moving direction (simultaneously)

-1 ± 2 g ± 1.5 g ± 1.0 g

NOTE: These limit load factors act simultaneously at the C.o.G. of the overall MGSE plus F/H assembly or of the F/H only. Acceleration positive direction is upwards. They represent the quasi-static loads, encompassing both the steady state and dynamic response contributions induced by conducting the described ground operations.

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8.4.2 Dynamic Loads

The dynamic environment experienced by MGSE Transport Containers during transportation of the F/H consists of sinusoidal and superimposed random vibrations as well as shock inputs as here after defined. A further contingent shock type input shall be considered due to mishandling and drop during loading/unloading operations. All these dynamic inputs are applicable for the attenuation system design of the MGSE Transport Containers in accordance to paragraph 7-1. M2-MGSE-REQ-1410 Sinusoidal Accelerations


Traces: Sinusoidal accelerations induced by transportation environment shall be as per following table:

Table 8-2 : Sinusoidal Acceleration Input

F (Hz) Acceleration/Amplitude 0.1 to 1 1 to 5 5 to 20

20 to 200 200 to 300

± 50 mm ± 8 mm

± 1.25 mm 2 g 3 g

NOTE: Sinusoidal accelerations, in input to the transport vehicle load bed, shall be considered acting simultaneously at 100% along vertical axis and 66% along each of longitudinal and lateral axes.

M2-MGSE-REQ-1420 Random Accelerations


Traces: Random accelerations, in input to the transport vehicle load bed, shall have following values in a log-log scale:

• 5 Hz ÷10 Hz, Spectral Power Density from 7.5E-04 g2/Hz to 3.0E-03 g2/Hz (+6 dB/oct) • 10 Hz ÷100 Hz, Spectral Power Density constant to 3.0E-03 g2/Hz • 100 Hz ÷200 Hz, Spectral Power Density from 3.0E-03 g2/Hz to 1.875E-04 g2/Hz

(-12 dB/oct) NOTE: These values are applicable to the three orthogonal axes one a time.

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M2-MGSE-REQ-1430 Shock Input


Traces: The following shock inputs due to the various transportation modes shall be considered:

• Road Transportation → 10 [g’s] for a duration of 20 ms (saw tooth or triangular form impulse) • Air Transportation → maximum 4.2 [g’s] for a duration of 20 ms (half-sinus form impulse)

M2-MGSE-REQ-1440 Drop Input


Traces: The shock input, due to a drop for mishandling of the Transport Container carrying the F/H, shall be considered equivalent to a fall from 100 mm height, when one edge of the container remains on the ground.

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9. PRODUCT ASSURANCE REQUIREMENTS

9.1 PA Safety Standard Requirements

MGSE are designed to take into account the specific Product Assurance and Safety standard requirements. M2-MGSE-REQ-1450 EU Safety Standard Rules


Traces: With particular reference to the RCS Filling and Pressurisation Equipment and MGSE used in potentially explosive atmospheres, the MGSE shall be designed and CE marked and certified respecting the National safety standard of the countries where the MGSE have to be used and EU directives at the latest issues, for instance: the Directive [RD 07] for low voltage, [RD 02] for machinery, [RD 06] for electromagnetic compatibility (according to paragraph 11.1.11.1 of [IR 0112] for Rover Module and ALD GSE and paragraph 11.1.8.1 of [IR 05008] for MGSE of all other F/H modules) and [RD 10] for MGSE subjected to ATEX normative, in addition to safety regulations of launcher Authority. The contractor shall identify for each product under his responsibility the applicability of the EU directives. Where applicable, the subcontractor shall perform the related certification towards the EU directives (e.g. machinery, electrical and electronic devices, pressurizing equipment etc.).

9.2 Reliability Requirements

The MGSE design will ensure that originated failure, directly or by propagation, shall not damage F/H or cause overstress F/H beyond procurement specification limit. The failure consequences and tolerance shall be quantified by their severity, which is a measure of the magnitude of the consequence. M2-MGSE-REQ-1460 Failure Consequence Severity


Traces: The severity of a failure consequence shall be classified according to the following scale:

• Catastrophic : loss of life, injury to personnel, long term detrimental environmental effects • Critical : loss of mission, short term detrimental environmental effects • Major : mission degradation (i.e., inability to provide the required performance) • Minor : all others

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M2-MGSE-REQ-1470 Failure Tolerance


Traces: All MGSE shall be designed to be zero failure tolerant for functional performance. Besides the MGSE shall be designed to be able to sustain:

• a single failure or operator error without catastrophic or critical consequences • any combination of two failures/operator errors without catastrophic consequences

Concerning the parts of the MGSE directly interfacing the F/H, a FMECA shall be carried out according to the requirements contained in paragraph 11.1.4 of [IR 0112] for Rover Module and ALD MGSE and same paragraph of [IR 05008] for MGSE of all other F/H modules.

M2-MGSE-REQ-1480 Redundancy Protection


Traces: Redundant major element of equipment (such as assemblies, panels, power supply, controls and associated interconnecting wires), shall be separated or otherwise protected, to ensure that an unexpected event that damages one, shall not likely prevent the other from performing normally (according to the requirements contained in paragraph 11.1.7 of [IR 0112] for Rover Module and ALD MGSE and paragraph 11.1.4 of [IR 05008] for MGSE of all other F/H modules).

9.3 Safety Factors

M2-MGSE-REQ-1490 Design and Proof Safety Factors


Traces: For the design and proof load test of the ExoMars MGSE items the safety factors reported in Table 7.1-1 shall apply. Assumed design safety factors and proof load factors are compliant to the [RD 01] and [RD A130].

9.4 Safety and Human Engineering

MGSE for ground operation will be designed, such that its operation in support of and in conjunction with flight hardware, does not result in hazard to the personnel, flight hardware or program ground facilities.

9.4.1 Safety Mechanical Requirements

The following mechanical provisions will be implemented to avoid injury to the personnel.

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M2-MGSE-REQ-1500 Suitable Guards


Traces: Manual/critical command/control which may cause personnel injury or equipment damage if inadvertently activated shall be provided with suitable guards.

M2-MGSE-REQ-1510 Touch Temperature Design


Traces: Accessible areas of F/H heated or cooled as a result of operation shall have a touch temperature not more than 45ºC or less than 4ºC.

M2-MGSE-REQ-1520 Protrusion


Traces: Protrusions which create a hazard such as hoses, brackets, etc., which cannot be eliminated by design, should be made to be removable during service or maintenance functions.

M2-MGSE-REQ-1530 Indices


Traces: All mechanical devices that require alignment or adjustment shall have indices to ensure proper alignment, adjustment and operation.

M2-MGSE-REQ-1540 Alignment Marks


Traces: Alignment indices or alignment marks shall be visible for alignment recheck without removal of any component.

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M2-MGSE-REQ-1550 Mechanical Stop


Traces: All mechanical actuating devices shall have definitive mechanical stops to prevent inadvertent lowering of the load (in case of lifting device) or protection against failures that could allow the device to exceed its intended limits of travel.

M2-MGSE-REQ-1560 Safe Working Load Display


Traces: All MGSE shall display a placard to identify the safe working load.

M2-MGSE-REQ-1570 Unintentional Movements


Traces: MGSE which is supported on wheels shall incorporate provisions to avoid unintentional movements.

M2-MGSE-REQ-1580 Sharp Edges and Corners


Traces: Sharp edges and corners that present a personnel safety hazard or potential damage to the equipment during usage shall be suitably protected or rounded.

M2-MGSE-REQ-1590 Clearances


Traces: All handles and controls including those for mechanism such as folding platforms shall be designed with sufficient clearances to adjacent structures or other components to prevent injury to fingers and hands.

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9.4.2 Hazard Control & Human Factor Requirements

MGSE design will make easy and safe the personnel operations. The design of the MGSE will include considerations of human engineering factors that affect human performance, as per requirements contained in [RD 02], [RD 03] and [RD 04]. The following hazard control measures will be adopted:

• Eliminate by design the potential for hazards (including those related to operations) • Minimise the severity of the hazard consequences • Incorporate safety and warning devices to control the hazard consequences • Develop and follow special procedures (i.e., emergency and contingency procedures) and training

An operational manual will be delivered for the correct and safe use of all the MGSE for the ExoMars F/H. M2-MGSE-REQ-1600 Human Engineering Criteria


Traces: Mainly the MGSE shall be designed to meet requirements in terms of: - Providing adequate space for man and his equipment to perform all the necessary operations and maintenance tasks, under both normal and emergency conditions - Using powered operation where necessary to avoid operator workload - Restricting maximum weight of components to be lifted by hand and maximum required force for hand operation. Above this limit, hoisting and actuation devices will be incorporated - Safety assurance through managing the risk from human error

M2-MGSE-REQ-1610 I/F Accessibility


Traces: The interface design of MGSE shall permit attachment and removal operations, providing access for hands and required tools with the necessary clearances.

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M2-MGSE-REQ-1620 Hand Limit Weight


Traces: Items weighing more than allowable value for handling/lifting by one person shall be prominently labelled identifying object weight and lift limitation (i.e. two person lift, three persons lift, etc.). Lifting shall be determined as follows: Handling Function Male and Female (kg) A

Lift an object from the floor and place it on a surface not higher than 1.5 m (about 5 ft) above the floor

16.8

B

Lift an object from the floor and place it on a surface not higher than 900 (about 36 in) above the floor

20.0

C Carry an object 10 m (33 ft) or less 19.0

M2-MGSE-REQ-1630 Hand Operation Limit Force

Verification: [EQP: A, I]

Traces: All MGSE components requiring actuation force greater than 100 N shall provide adequate support devices to reduce the necessary force within 100 N.

M2-MGSE-REQ-1640 Sling & Lifting Accessories Provi sions


Traces: In case of item handled by crane, slings and lifting accessories of the hoisting points (such as wire ropes, belts, rings, eyebolts, shackles, hooks, etc..) it shall be delivered provided with adequate proof load certificate.

M2-MGSE-REQ-1650 Warning Placards


Traces: All equipment, including shipping containers, shall have warning placards at visible locations to identify hazardous commodities and restrictions such as "No Smoking", "Explosives", etc…

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M2-MGSE-REQ-1660 Indicators & Control Labels


Traces: All controls and indicators shall be clearly marked or labeled to indicate system functions.

M2-MGSE-REQ-1670 Potential Hazard Prevention


Traces: The MGSE design shall incorporate appropriate feature (redundancies, inhibits, etc...) to eliminate or reduce and control all potential hazards.

M2-MGSE-REQ-1680 Hazard Prevention by Design Impro vement


Traces: Design improvement applied to eliminate or reduce and control hazards shall be subjected to Customer approval.

M2-MGSE-REQ-1690 Warning Labels for Command/Contro l


Traces: Commands and controls shall be easily used from a human interface standpoint, but their inadvertent actuation shall be avoided, via the introduction of warning labels and protective guards.

M2-MGSE-REQ-1700 Display and Control Location


Traces: Display and controls shall be located and labelled to ensure quick identification. Warning labels shall identify the type of hazard and the action that would prevent its occurrence.

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M2-MGSE-REQ-1710 Instruction Labels Readability


Traces: All characters on instruction panels, warning labels and warning placards shall be placed in clearly visible locations and shall be easily readable.

M2-MGSE-REQ-1720 Alarm/Emergency Indicators


Traces: Where applicable, an emergency red coloured “OFF” push button shall be used to switch off the system power supply, mounted in visible manner on the cabinet front face. It shall have reset capability.

M2-MGSE-REQ-1730 Equipment Control Position


Traces: Where possible, equipment controls and displays shall be positioned in front of the equipment itself, except where safety requirements dictate that they shall be positioned at the rear. Where possible, equipments which must be used frequently (excluding operator consoles) shall be positioned in a rack such that they can be easily operated by a person in a standing position.

M2-MGSE-REQ-1740 Control/Display Association


Traces: When controls and displays are not located one close to the other (e.g. displays are an in upper area and controls in a lower area), the controls shall be located in same relative position as their associated displays.

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M2-MGSE-REQ-1750 Control/Display Adjustment


Traces: Controls and displays requiring fine adjustment and accurate readout shall be located close to the operator normal line of sight. Safety controls that must be operated in specific sequence shall be sequentially interlocked.

M2-MGSE-REQ-1760 Emergency Control


Traces: Emergency controls (electrical or mechanical) used for shutdown, saving, alarm or corrective action shall be clearly marked, visible and readily accessible to operating personnel.

M2-MGSE-REQ-1770 Display Scales


Traces: Display scales shall be provided with sufficient graduation to read the required accuracy without interpolation. Marking and labels shall utilize international standard/symbols, as per [RD 02], [RD 03] and [RD 04].

M2-MGSE-REQ-1780 Marking Language


Traces: All operational data, controls, displays, internal and external markings shall be in English.

MS-MGSE-REQ-1790 Weight/CoG Identification


Traces: Gross weight and CoG shall be conspicuously identified on all equipment required to be lifted or moved by forklifts, hoists, cranes and similar handling equipment.

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M2-MGSE-REQ-1800 Hoisting Point Identification


Traces: Hoisting points and tie-down points shall be clearly marked or labelled.

M2-MGSE-REQ-1810 Hoisting Device Reassembly


Traces: All hoisting load bearing components which are normally disassembled, such as, individual slings, cables, shackles, pins, bolts, and similar parts shall be tethered, serialised, tagged, or marked for positive identification to assure proper assembly.

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9.5 Cleanliness

M2-MGSE-REQ-1820 Prevent contamination ISO 8


Traces: AIV Requirement Document #AIV-VER-310 The MGSE shall be designed to operate inside an ISO 8 clean room without causing contamination to the F/H or to the facility.

M2-MGSE-REQ-1830 Prevent contamination ISO 7 HC


Traces: AIV Requirement Document #AIV-VER-310 The MGSE shall be designed to operate inside an ISO 7 HC clean room without causing contamination to the F/H or to the facility.

M2-MGSE-REQ-1840 Prevent contamination ISO 3 AMC-9


Traces: AIV Requirement Document #AIV-VER-310 The MGSE shall be designed to operate inside an ISO 3 AMC-9 environment without causing contamination to the F/H or to the facility.

M2-MGSE-REQ-1850 MGSE General Cleanliness Level


Traces: The MGSE to be used in ISO 8 and ISO 7HC clean rooms shall be delivered to TASI at Highly Sensitive Visible Clean (HSVC) cleanliness level as defined in [ES 104].

M2-MGSE-REQ-1860 Cleanliness Certification


Traces: All MGSE shall be accompanied by dedicated “Certification of Cleanliness” upon delivery.

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M2-MGSE-REQ-1870 MGSE Design for Cleanability


Traces: The MGSE design shall minimize holes and dust traps in order to make cleaning easier:

• smooth surfaces (0.8 mm Ra or Rms ≤ 3 µm), • easy access to surfaces to be cleaned, • avoidance of sharp corners (i.e. fillet radius higher than 3 mm)

M2-MGSE-REQ-1880 MGSE Design Oriented to Preservat ion of Flight H/W Ultracleanliness


Traces: AIV Requirement Document #AIV-VER-310 The design of all ALD MGSE to be used in the ISO3/AMC-9 environment shall foresee suitable mounting brackets/flanges to mount double biobags allowing the Cleanliness preservation of the Isolator Environment. The MGSE design must be compatible with double Bags, i.e. the nominal performance of the MGSE must be guaranteed when the double bags are mounted.

M2-MGSE-REQ-1890 GSE Contamination Level


Traces: AIV Requirement Document #AIV-VER-310 The GSE (i.e. for RCS Filling/Pressurisation or for UCZ pressurization and purging) shall be made of materials not introducing any contamination risk for the fluid. The cleanliness level of the GSE inner circuit shall be the same of the F/H which the GSE interfaces to.

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M2-MGSE-REQ-1900 Material and Processes Cleanlines s Requirements


Traces: MGSE shall be made of materials and surface protection treatments compatible with the cleaning agents. In particular:

- MGSE entering the ISO 8 and ISO 7 HC shall be at least compatible with IPA wiping - MGSE entering the ISO3/AMC-9 environment shall be compatible with UltraSonic Bath in

solvents (Acetone, IPA, Chloroform) and with the Accelerated CO2 Snow Cleaning treatment. Note 1: see Planetary Protection Requirements M2-MGSE-REQ-1910 MGSE UltraCleaning for ISO 3/AMC- 9 Environment


Traces:

MGSE parts entering the ISO3/AMC-9 environment coming in contact with UltraClean H/W shall be submitted to the same UltraCleaning Treatment foreseen for the Flight H/W pertaining to the UCZ and shall be cleaned to the same MOC and PAC levels foreseen for the flight H/W. M2-MGSE-REQ-1920 MGSE Design for Ultracleaning


Traces: MGSE to be UltraCleaned (i.e. entering the ISO3/AMC-9 environment) shall be dismountable in loose parts not bigger than 80x80x80 cm (TBC).

Comment [m2]: Questo requisito (come anche quello che chiede che i GSE siano allo stesso livello del Flight H/W, sono già presenti nella CRS EXM-RM-SSR-AI-0015 ed anche nella CRS 2018. Almeno per questo, possiamo forse puntare al Req della CRS 0015, che però non è applicabile a tutto il sistema, ma d’altronde interessa solo il sistema RM

Comment [m3]: Questo serve affinchè le parti possano entrare nel bagno ultrasonico, ma sulle dimensioni ci devo ragionare ancora un attimo e avere info sul bagno più grande che riusciamo ad avere (e che entri nell’isolatore)

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10. VERIFICATION REQUIREMENTS

The verification program for the ExoMars F/H MGSE will be developed and conducted by Contractors to demonstrate conformance to the applicable requirements. A satisfactory completion of the verification process is the basis for a contractual acceptance of the product by the customer. Requirements contained in this document as well as requirements in the dedicated and applicable equipment requirements specification indicated by the identification and numbering scheme explained below shall be subjected to formal verification close out. The verification process includes definition of detailed verification requirements, verification planning, conduct, assessment and reporting.

10.1 Acceptance Verification

Acceptance verifications are those formal verifications that are conducted to assure that the equipment meets the contracted or design requirements. Formal verification of performance characteristics occurs for nominal operational and critical physical requirements during acceptance. Acceptance will be accomplished to verify compliance with deliverable end item, interface documentation, and other contract requirements.

10.2 Verification Methods

The verification methods will be Test, Analysis, Inspection, Review of Design and Similarity. The allocation of these methods is based upon design analyses, complexity of the item, criticality category and associated cost.

10.2.1 Review of Design

The Review of Design is the verification by validation of previous correlated records, certifications, test verification reports, reports, technical descriptions, engineering drawings, etc., showing un-ambiguously that the requirements are satisfied.

10.2.2 Analysis

Verification by analysis is a process used in lieu of, or in addition to, other verification methods to verify compliance to specification requirements. It will include, but will not be limited to, engineering analysis, statistics and qualitative analysis, computer and hardware simulation and analog modeling. Analytical calculations will be carried out in order to evaluate the mass, CoG and MoI (if needed) of the used F/H segment element dummies. Stress analysis will be carried out on each item used to handle/transport flight hardware using specified load cases. Stress analysis will not be performed for items from a supplier standard range (however the recommended load/rating for these items will not be exceeded). A dynamic analysis shall be performed on vibration isolation system of the shipping containers and for evaluation of eigen-frequencies of the vibration adapters. A thermal analysis will be performed for the thermal test adapters and for the shipping containers. In principle, the design margins will be achieved by analysis (and validated by appropriate tests).

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10.2.3 Inspection

Inspection is a method of verification that determines conformance to requirements without the use of special laboratory equipment, procedures, test support items or services. Verification by inspection will be conducted by standard quality control methods to verify compliance with requirements of construction features, document and drawing compliance, workmanship standards and physical condition.

10.2.4 Test

Testing is selected as the prime method of requirement verification. M2-MGSE-REQ-1930 Acceptance Testing


Traces: Each MGSE item shall be subjected to acceptance testing as part of its verification process: the required approach shall be aimed to demonstrate that the MGSE item is free from material and workmanship defects, to deeply evaluate the design approach, and finally to verify the compliance with the design requirements.

M2-MGSE-REQ-1940 Test Procedure


Traces: Test procedures shall be prepared and delivered for each MGSE. They shall contain test planning and any other information to perform Acceptance Tests accordingly.

M2-MGSE-REQ-1950 Test Conditions


Traces: Test condition, test parameters tolerance, accuracy of test apparatus and test success criteria shall be defined in each MGSE test procedure.

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M2-MGSE-REQ-1960 Test Report


Traces: Test Reports shall be provided for the formal requirement verification close out. The test measured parameters and plots results (if any) shall be recorded and annexed in the Test Report.

10.2.4.1 Acceptance Test Description

A brief description of typical acceptance tests carried out on the MGSE is here after reported. M2-MGSE-REQ-1970 Dimensional and Fit Check


Traces: The test shall consist of dimension measurements to verify the compliance to the design, the capability to be assembled and the compliance with the interface requirements. For the mass dummies measurement of flatness and roughness of their base plate (I/F with the F/H) shall be also performed.

M2-MGSE-REQ-1980 MGSE Mass and CoG Determination


Traces: The MGSE mass shall be determined by weighing. Mass of dummies shall be accurately measured by weighing. Coordinate of MGSE and mass dummies CoG, if not determinable by test, shall be provided by analysis.

M2-MGSE-REQ-1990 Non Destructive Inspection


Traces: Magnetic particle, dye penetrant or other suitable crack detecting test shall be performed, before and after static proof load, on all manufactured and commercial lifting components (such as pins, lugs and fork ends, eyebolts, shackles, rings, turnbuckles, etc.) and on critical welds (if any).

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M2-MGSE-REQ-2000 Static Load Test


Traces: The static proof load tests shall be conducted to verify the strength capability of the MGSE in the worst loading condition. Particularly the MGSE to Flight Hardware I/F’s shall be proofed. In general the static load test will be performed following the here below procedure: • use the mass dummy, configured in such a way to be representative of the F/H interfaces, the proof mass (design mass increased of the proof factor required by the specification) and CoG in the heaviest loading condition • assemble the test set-up • perform dimensional check of the unloaded MGSE (if necessary) • execute the proof load for a minimum time period of five minutes • perform visual inspection and dimensional check (if any) after the test For some MGSE the static load test could be also conducted simulating the proof load in other way, without using the mass dummies.

M2-MGSE-REQ-2010 Functional/Performance Test


Traces: This test, executed after the proof load, shall demonstrate compliance to the MGSE operative performances with the specification requirements. The mass dummy shall be configured to be representative of the nominal mass, CoG and interfaces of the handled F/H, in the worst loading condition. Proper functional test shall be carried out to certify the performance requirements of the F/H container air conditioning system (if any).

M2-MGSE-REQ-2020 EMC tests (as applicable)


Traces: This test shall consist on performing an EMC "sniffing" test to determine the possible electromagnetic effects.

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M2-MGSE-REQ-2030 Electrical Bonding Test


Traces: The bonding test shall verify the effective high electrical conductivity between the F/H and the supporting MGSE and between MGSE and facility grounding network. The resistance across the interfaces, measured by a direct current of 10 mA, shall be less than 50 mΩ.

M2-MGSE-REQ-2040 Leak Test


Traces: Scope of the test shall be to verify the capability of the F/H Transport Container of:

• maintaining the system in over pressure during the transportation and storage as per relevant requirements • being water tight • support, with a minimum intervention of sealing implementation (if needed), the test of propulsion sub-system overall leak test

M2-MGSE-REQ-2050 Drop Test


Traces: Scope of the test shall be to verify that the F/H, when handled or transported inside the transport container, is isolated against shock to the specified level. The test will be performed with the container loaded by a mass dummy representative of the F/H mass, CoG and I/F. The container will be subjected to two or more drop test, as per Table 516.6-VI of Method 516.6, of [RD 11]. Acceleration along the three axes shall be measured near the CoG of the F/H mass dummy. The acceleration values exceeding the flight hardware allowable levels shall be considered a test failure.

REFERENCE : DATE :


ISSUE : 01 PAGE : 77/101




11. DOCUMENTATION

The documentation delivered by the contractor will respect the following requirements. M2-MGSE-REQ-2060 Documentation Language


Traces: The documentation delivered by the supplier shall be in English language and shall comply to the requirements in [IR 020].

M2-MGSE-REQ-2070 Supplied Documentation


Traces: In addition to the documentation requirements of the applicable Statement of Work or purchase order, the contractor shall deliver as a minimum the following documentation:

• CIDL • Safety Data Package (Ground) • Assembly and ICD Drawings • Design Report (including Analysis Report and Test Plan) • Test Procedures • User/Operation & Maintenance Manual • Verification Reports (Test Reports, Inspection Reports, etc..) • VCD • Acceptance Data Package (including C.O.C., NCR status list, etc..)

M2-MGSE-REQ-2080 Document Format


Traces: The delivered documentation format shall be compliant to requirements specified in [IR 020].

REFERENCE : DATE :


ISSUE : 01 PAGE : 78/101




12. PREPARATION FOR DELIVERY

12.1 MGSE Shipping and Reusable Container

M2-MGSE-REQ-2090 MGSE Shipping and Reusable Contai ner


Traces: All MGSE items (with exception of Transport Container MGSE) shall be delivered with shipping containers (and associated slings for container handling, if any), compatible with air, rail, sea and road transportation rules and means. Packaging, handling, storage and transportation of assemblies and equipment, shall be performed in accordance to detailed procedures approved by the customer.

M2-MGSE-REQ-2100 Commercial Containers


Traces: Commercial reusable containers, when demonstrated to meet the F/H programme requirements, shall be used to the maximum extent to reduce package design and fabrication costs.

M2-MGSE-REQ-2110 Storage Periods


Traces: Containers that will require storage on-ground shall be designed to remain serviceable at designed performance levels throughout foreseen storage periods.

M2-MGSE-REQ-2120 Wooden Containers


Traces: Wooden container shall be subjected to a fumigation treatment as per [RD 08].

REFERENCE : DATE :


ISSUE : 01 PAGE : 79/101




12.2 Shipping and Reusable Container Design Perform ances

M2-MGSE-REQ-2130 Shipping Container Manufacturing Material


Traces: The shipping containers shall be manufactured by materials resistant to degradation in reliability, safety and performance due to natural/induced environment specified in paragraph. 8.0 of this specification (especially un-flammable materials and, if any, flame retardant and water repellent paints) .

M2-MGSE-REQ-2140 Packing Materials


Traces: Packing materials, shall not release corrosive vapour (such those from polyvinylchloride, neoprene, vinyl and polysulphide) or contain corrosive constituents.

M2-MGSE-REQ-2115 Packing Cleanliness Capability

Verification: [EQP: RoD] Traces The packaing material shall be able to maintain the Visible Clean cleanliness level of the MGSE at the delivery.

M2-MGSE-REQ-2160 Containers Colour


Traces: The basic containers colour shall be white.

REFERENCE : DATE :


ISSUE : 01 PAGE : 80/101




12.3 Shipping and Reusable Container Provisions

M2-MGSE-REQ-2170 Protection


Traces: The shipping containers shall provide any dedicated protection to avoid damages to the MGSE.

M2-MGSE-REQ-2180 MGSE Internal Locking


Traces: The shipping container shall provide means to assure an inside safe locking of the MGSE on the container base.

M2-MGSE-REQ-2190 Tie-down Provisions


Traces: Tie-down provisions shall be foreseen on the shipping containers for securing to the transportation means.

M2-MGSE-REQ-2200 Protective Covers


Traces: Contractor shall define the need of protective covers to avoid MGSE damage/cleanliness during storage/transportation.

M2-MGSE-REQ-2210 Waterproof Capability


Traces: The shipping containers shall be splash waterproof.

REFERENCE : DATE :


ISSUE : 01 PAGE : 81/101




M2-MGSE-REQ-2220 Desiccant Salts


Traces: The shipping containers shall be provided of dedicated sites for housing a sufficient amount of hygroscopic salt bags.

M2-MGSE-REQ-2230 Handling Provisions

Verification: [EQP: T, I]

Traces: The shipping containers with a mass greater than 30 kg shall have adequate provisions for hoisting by sling and/or forklift.

M2-MGSE-REQ-2240 Cover Lid Handling Provisions


Traces: The shipping container cover lid with a mass greater than 30 kg shall have adequate handling points for lifting by sling.

M2-MGSE-REQ-2250 Containers Handles


Traces: Light MGSE containers and relevant cover lids (with a mass less than 30 kg) shall be equipped with handles at least placed at two opposite faces.

M2-MGSE-REQ-2260 Containers Closing and Opening De vices


Traces: MGSE containers shall be equipped with protected clamps or latches for closing and opening.

REFERENCE : DATE :


ISSUE : 01 PAGE : 82/101




M2-MGSE-REQ-2270 Containers Shock Indicator


Traces: MGSE containers shall be equipped with shock indicator equipment (peak level sufficient).

M2-MGSE-REQ-2280 Containers Dimensions


Traces: MGSE containers maximum height and width (outside dimension) shall be 2.5 m.

M2-MGSE-REQ-2290 Un-packaging Tools


Traces: Packaging shall be such that unpacking with existing tools is feasible.

12.4 Shipping and Reusable Containers Marking

M2-MGSE-REQ-2300 Transport Container Marking


Traces: The shipping containers shall be marked and labelled in English including following marking necessary to ensure safe condition to the personnel, F/H and facilities: • project/program identification • MGSE content nomenclature/identification • MGSE part number • container part number • container serial number • container net and gross weight • container CoG (empty) • container plus MGSE total CoG • Safe Working Load • container overall dimensions • lifting points identification • special safety instruction marking/labels (as needed) • stackable (or not) container marking • bonding point identification (if necessary)

REFERENCE : DATE :


ISSUE : 01 PAGE : 83/101




M2-MGSE-REQ-2310 Contract


Traces: All shipping document shall clearly refer to the applicable contract.

M2-MGSE-REQ-2320 Container Label Position


Traces: Each container shall be labelled on four sides plus top. Complete marking shall be at least on one side.

M2-MGSE-REQ-2330 Container Annexed Documentation


Traces: The MGSE containers shall be designed in such a way to be portable together with related documentation, spare parts and all support instrumentation (if any).

REFERENCE : DATE :


ISSUE : 01 PAGE : 84/101




13. PLANETARY PROTECTION IMPLEMENTATION REQUIREMENTS

13.1 Introduction

All MGSE hardware shall respect the PP implementation requirements here after defined.

13.2 PP Requirements for MGSE to be introduced in t he ISO 7HC Clean Room

M2-PP-REQ-0010 Subco Operators Training by P-PPE

Verification: [EQP: T, RoD, I]

Traces: All personnel directly (e.g.: AIT operators) or indirectly (e.g.: supervisors) involved with controlled environments shall be trained in Planetary Protection by the Prime and certified by the P-PPE.

M2-PP-REQ-0020 MGSE Compatibility with IPA Wiping


Traces: The MGSE shall be compatible with 70 % Isopropyl alcohol (IPA) wiping. Note 1: not epoxy paints have to be used due to after a number of IPA wipes the epoxy comes off if not mixed, applied or cured properly. Note 2: powder coated steel is compatible with IPA cleaning

M2-PP-REQ-0030 MGSE Design Accessible to IPA Wipin g


Traces: The MGSE design shall allow an easy access at the surfaces to be cleaned with IPA wiping.

M2-PP-REQ-0040 MGSE Compatibility with Bioburden A ssays


Traces: The MGSE shall be compatible with steril water damp assays (swabs and wipes).

REFERENCE : DATE :


ISSUE : 01 PAGE : 85/101




M2-PP-REQ-0050 MGSE Design Accessible to Assays


Traces: The MGSE design shall allow an easy access at the surfaces to be assayed.

M2-PP-REQ-0060 MGSE Material List and Relevant Dat a Sheets


Traces: The complete list constituent materials of the MGSE coming in contact with flight hardware shall be provided to PPE. Material data sheets shall include at least the following features:

• Identifier (e.g.: Trade Mark, MAPTIS code,…) • Rating and references for flammability, off-gassing and fungus growth • Organic material list

M2-PP-REQ-0070 Fluids in contact with MGSE


Traces: All liquids and gases that will be in contact with the Bioburden controlled flight hardware shall be filtered through 0.2 µm porous.

M2-PP-REQ-0080 MGSE Cleaning before Delivery to TA SI


Traces: Before delivering to TASI, the MGSE shall be cleaned with steril 70% IPA (Isopropyl alcohol) up to Highly Sensitive Visible Clean (HSVC) level, as defined in paragraphs 3.2.25 and 3.2.28 of ECSS-Q-ST-70-50C [ES 104].

REFERENCE : DATE :


ISSUE : 01 PAGE : 86/101




13.3 PP Requirements for MGSE to be introduced in the ISO 3 AMC-9 Clean Room

M2-PP-REQ-0090 Subco Operators Training by P-PPE

Verification: [EQP: T, RoD, I]

Traces: All personnel directly (e.g.: AIT operators) or indirectly (e.g.: supervisors) involved with controlled environments shall be trained in Planetary Protection by the Prime and certified by the P-PPE.

M2-PP-REQ-0100 MGSE Compatibility with IPA Wiping


Traces: The MGSE shall be compatible with 70 % Isopropyl alcohol (IPA) wiping. Note 1: not epoxy paints have to be used due to after a number of IPA wipes the epoxy comes off if not mixed, applied or cured properly. Note 2: powder coated steel is compatible with IPA cleaning

M2-PP-REQ-0110 MGSE Design Accessible to IPA Wipin g


Traces: The MGSE design shall allow an easy access at the surfaces to be cleaned with IPA wiping.

M2-PP-REQ-0120 MGSE Compatibility with Bioburden A ssays


Traces: The MGSE shall be compatible with steril water damp assays (swabs and wipes).

REFERENCE : DATE :


ISSUE : 01 PAGE : 87/101




M2-PP-REQ-0130 MGSE Design Accessible to Assays


Traces: The MGSE design shall allow an easy access at the surfaces to be assayed.

M2-PP-REQ-0140 MGSE Material List and Relevant Dat a Sheets


Traces: The complete list constituent materials of the MGSE coming in contact with flight hardware shall be provided to PPE. Material data sheets shall include at least the following features:

• Identifier (e.g.: Trade Mark, MAPTIS code,…) • Rating and references for flammability, off-gassing and fungus growth • Organic material list

M2-PP-REQ-0150 Fluids in contac t with MGSE


Traces: All liquids and gases that will be in contact with the Bioburden controlled flight hardware shall be filtered through 0.2 µm porous. M2-PP-REQ-0160 MGSE Cleaning before Delivery to TA SI


Traces: Before delivering to TASI, the MGSE shall be cleaned with steril 70% IPA (Isopropyl alcohol) up to Highly Sensitive Visible Clean (HSVC) level, as defined in paragraphs 3.2.25 and 3.2.28 of ECSS-Q-ST-70-50C [ES 104].

REFERENCE : DATE :


ISSUE : 01 PAGE : 88/101




M2-PP-REQ-0170 MGSE Compatibility with Sterilizati on Process DHMR

Vérification: [EQP: A, RoD]

Traces: The MGSE shall be compatible with the Dry Heat Microbial Reduction process (DHMR) to be performed in accordance to the following parameters: Temperature: 125ºC Time: 6 hours Humidity: 1.2 water g/m3

M2-PP-REQ-0180 MGSE DHMR Cycles

Vérification: [EQP: A, RoD]

Traces: The MGSE shall be compatible with at least 3 sterilization cycles of Dry Heat Microbial Reduction process (DHMR) to be performed in accordance to sterilization parameters of MS-PP-REQ-0170. M2-PP-REQ-0190 MGSE Limit Dimensions

Vérification: [EQP: RoD]

Traces: The MGSE or the MGSE disassembled part shall be able to be sterilized in an oven with an internal chamber of the following dimensions: 1.3 m (width) x 1.0m (length) x 0.8m (height).

REFERENCE : DATE :


ISSUE : 01 PAGE : 89/101




14. ANNEX 1: EXM-M2-SSR-AI-0033 VERSUS ALD MGSE APPLICABILITY MATRIX

REFERENCE : DATE :


ISSUE : 01 PAGE : 90/101




PUID Object Short Text

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[M2-MGSE-REQ-0010]

Items Standardization X X X X X X X X

[M2-MGSE-REQ-0020]

Installation X X X X X X

[M2-MGSE-REQ-0030]

Interface Functional Capability X X X X X X

[M2-MGSE-REQ-0040]

Unplanned Movements X X X X X X

[M2-MGSE-REQ-0050]

I/F Loads X X X

[M2-MGSE-REQ-0060]

Mating/De-mating X X X X X X

[M2-MGSE-REQ-0070]

Cleanliness X X X X X X X X

[M2-MGSE-REQ-0080]

Clearance X X X

[M2-MGSE-REQ-0090]

Special Tools X X X

[M2-MGSE-REQ-0100]

Adjustment X X X X X X

[M2-MGSE-REQ-0110]

Assembly Inspection X X X X

[M2-MGSE-REQ-0120]

Re-assembly Instructions X X X X

[M2-MGSE-REQ-0130]

Hand Lifted Max Weight X X X X X X X

[M2-MGSE-REQ-0140]

Lifting Point Marking X X X X X X X

[M2-MGSE-REQ-0150]

Stability X X X X X

[M2-MGSE-REQ-0160]

Parking X X X X X

[M2-MGSE-REQ-0170]

Displacements Provisions X X X X X

[M2-MGSE-REQ-0180]

Useful Life X X X X X X X X

[M2-MGSE-REQ-0190]

Limited Life Item X X X X X X X X

[M2-MGSE-REQ-0200]

Limited Life Item Utilization Exception X X X X X X X X

[M2-MGSE-REQ-0210]

Limited Life Item List X X X X X X X X

[M2-MGSE-REQ-0220]

Maintainability X X X X X X X X

[M2-MGSE-REQ-0230]

Maintenance Unavailability Period X X X X X X X X

[M2-MGSE-REQ-0240]

Failure Unavailability Period X X X X X X X

REFERENCE : DATE :


ISSUE : 01 PAGE : 91/101





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[M2-MGSE-REQ-0250]

Protection for Personnel X X X X X X X

[M2-MGSE-REQ-0260]

Replacement X X X X X X X

[M2-MGSE-REQ-0270]

Preventive Maintenance X X X X X X X

[M2-MGSE-REQ-0280]

On-line Maintenance X X X X X X X

[M2-MGSE-REQ-0290]

Off-line Repair X X X X X X X

[M2-MGSE-REQ-0300]

Spare Number X X X X X X X

[M2-MGSE-REQ-0310]

Consumable Spare X X X X X X X

[M2-MGSE-REQ-0320]

Spare Tool X X X X X X X

[M2-MGSE-REQ-0330]

Accessibility X X X X X X X

[M2-MGSE-REQ-0340]

Replaceable Component X X X X X X X

[M2-MGSE-REQ-0350]

Standardization Tools & Fixtures X X X X X X X

[M2-MGSE-REQ-0360]

Torque and Special Tools X X X X X X X

[M2-MGSE-REQ-0370]

Transportation Provisions X X X X X X X

[M2-MGSE-REQ-0380]

Dimension Constraints X X X X X X X

[M2-MGSE-REQ-0390]

Part Numbering X X X X X X X

[M2-MGSE-REQ-0400]

MGSE Identification X X X X X X X

[M2-MGSE-REQ-0410]

MGSE Labeling X X X X X X X

[M2-MGSE-REQ-0420]

Marking Lifetime X X X X X X X

[M2-MGSE-REQ-0430]

Marking Techniques X X X X X X X

[M2-MGSE-REQ-0440]

Hoisting Points Identification X X X X

[M2-MGSE-REQ-0450]

Control of Lifting MGSE Re-Assembly X X X

[M2-MGSE-REQ-0460]

Workmanship X X X X X X X

[M2-MGSE-REQ-0470]

I/F to Flight Hardware X X X X X X

[M2-MGSE-REQ-0480]

I/F Contact Material X X X X X X

REFERENCE : DATE :


ISSUE : 01 PAGE : 92/101





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[M2-MGSE-REQ-0490]

I/F to Facilities X X X X X X X

[M2-MGSE-REQ-0500]

I/F to Integration Facilities X X X X X X X

[M2-MGSE-REQ-0510]

I/F to Test Facilities X X X

[M2-MGSE-REQ-0520]

Electrical Power Supply I/F

[M2-MGSE-REQ-0530]

GN2 Connection I/F X

[M2-MGSE-REQ-0540]

I/F to EDU

[M2-MGSE-REQ-0550]

Wheels Provisions X X

[M2-MGSE-REQ-0560]

Container to Transportation Means I/F X X X X X X X

[M2-MGSE-REQ-0570]

Compliance to Transportation Standard Rules

X X X X X X X

[M2-MGSE-REQ-0580]

I/F to Standard Transportation Means X X X X X X X

[M2-MGSE-REQ-0590]

I/F to Road Transport X X X X X X X

[M2-MGSE-REQ-0600]

I/F to Air Transport X X X X X X X

[M2-MGSE-REQ-0610]

International System Measurement Unit X X X X X X X X

[M2-MGSE-REQ-0620]

Coordinate System & Reference Marks X X X X X X

[M2-MGSE-REQ-0630]

Design Normative X X X X X X X

[M2-MGSE-REQ-0640]

MGSE Weight and Size X X X X X X X

[M2-MGSE-REQ-0650]

Load Environment X X X X X X X

[M2-MGSE-REQ-0660]

Safety Factors X X X X X X X

[M2-MGSE-REQ-0670]

De-coupling Requirements X

[M2-MGSE-REQ-0680]

Design Criteria X

[M2-MGSE-REQ-0690]

Random Acceleration Amplitude X

[M2-MGSE-REQ-0700]

Vibration Combination Method X

[M2-MGSE-REQ-0710]

Transport Shock Response X

[M2-MGSE-REQ-0720]

Drop Shock Response X

REFERENCE : DATE :


ISSUE : 01 PAGE : 93/101





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[M2-MGSE-REQ-0730]

Manufacturing Material General Requirements

X X X X X X X X

[M2-MGSE-REQ-0740]

Commercial Material X X X X X X X X

[M2-MGSE-REQ-0750]

Structural Metallic Material X X X X X X X X

[M2-MGSE-REQ-0760]

Connection Hardware Material X X X X X X X X

[M2-MGSE-REQ-0770]

Non Metallic Material X X X X X X X X

[M2-MGSE-REQ-0780]

Material Restrictions X X X X X X X X

[M2-MGSE-REQ-0790]

Shatterable Material X X X X X X X X

[M2-MGSE-REQ-0800]

Flammability Requirements X X X X X X X X

[M2-MGSE-REQ-0810]

Fungus Resistance X X X X X X X X

[M2-MGSE-REQ-0820]

Corrosion X X X X X X X X

[M2-MGSE-REQ-0830]

Dissimilar Metal Assembly X X X X X X X

[M2-MGSE-REQ-0840]

Material Non Destructive Inspection (NDI) X X X X X X X

[M2-MGSE-REQ-0850]

Critical Welds X X X X X X X

[M2-MGSE-REQ-0860]

Critical Weld Identification X X X X X X X

[M2-MGSE-REQ-0870]

Protective Coatings and Finishes X X X X X X X X

[M2-MGSE-REQ-0880]

Electrical Design General Requirements

[M2-MGSE-REQ-0890]

Power Supply

[M2-MGSE-REQ-0900]

Receptacles and Plugs

[M2-MGSE-REQ-0910]

Electrical & Electronic Safety Normative

[M2-MGSE-REQ-0920]

Electrical Safety Protections

[M2-MGSE-REQ-0930]

Operating Voltage Indication

[M2-MGSE-REQ-0940]

“Explosion Proofed” Requirement

[M2-MGSE-REQ-0950]

Electrical Equipment Control Safety Provisions

[M2-MGSE-REQ-0960]

Electrical Contact Resistance X X X X X X X

REFERENCE : DATE :


ISSUE : 01 PAGE : 94/101





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[M2-MGSE-REQ-0970]

Electromagnetic Compatibility

[M2-MGSE-REQ-0980]

Electrical Motor

[M2-MGSE-REQ-0990]

Electrical Motor Insulation

[M2-MGSE-REQ-1000]

F/H Insulation from Crane X X

[M2-MGSE-REQ-1010]

Power Loss Safety Device

[M2-MGSE-REQ-1020]

Power-Kill Safety Switch

[M2-MGSE-REQ-1030]

Grounding Point Provisions X X X X X

[M2-MGSE-REQ-1040]

Grounding Connections X X X X X

[M2-MGSE-REQ-1050]

Bonding Straps & Jumpers X X X X X

[M2-MGSE-REQ-1060]

Grounding Characteristic for EMC X X X X X

[M2-MGSE-REQ-1070]

Mobile Equipment Grounding Provisions

[M2-MGSE-REQ-1080]

MGSE Grounding Resistance Features X X X X X

[M2-MGSE-REQ-1090]

Grounding Cable Length X X X X X

[M2-MGSE-REQ-1100]

Electrical Resistance from MGSE to Facility Grounding

X X X X X

[M2-MGSE-REQ-1110]

Cable and Connector Installation Features

[M2-MGSE-REQ-1120]

Solid Wire

[M2-MGSE-REQ-1130]

Cable and Wire Marking

[M2-MGSE-REQ-1140]

Cable and Wire Clamping

[M2-MGSE-REQ-1150]

Wires Insulation

[M2-MGSE-REQ-1160]

Cable Protection

[M2-MGSE-REQ-1170]

Power Connector

[M2-MGSE-REQ-1180]

Switch Marking

[M2-MGSE-REQ-1190]

Electr. Comp. Safety Design Precautions

[M2-MGSE-REQ-1200]

Visual Provisions

REFERENCE : DATE :


ISSUE : 01 PAGE : 95/101





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[M2-MGSE-REQ-1210]

Electrical Parameters Indication

[M2-MGSE-REQ-1220]

Overload Protection Provisions

[M2-MGSE-REQ-1230]

Circuit Breakers Trip Provisions

[M2-MGSE-REQ-1240]

Overload Protection Installation

[M2-MGSE-REQ-1250]

Circuit Breaker Setting Indication

[M2-MGSE-REQ-1260]

Circuit Breakers Sizing

[M2-MGSE-REQ-1270]

Overload Protection Device Sizing

[M2-MGSE-REQ-1280]

Temperature X X X X X X X X

[M2-MGSE-REQ-1290]

Humidity X X X X X X X X

[M2-MGSE-REQ-1300]

Pressure X X X X X X X X

[M2-MGSE-REQ-1310]

Facility Environment Cleanliness X X X X X X X X

[M2-MGSE-REQ-1320]

Temperature X

[M2-MGSE-REQ-1330]

Humidity X

[M2-MGSE-REQ-1340]

Pressure X

[M2-MGSE-REQ-1350]

Outdoor Environment Cleanliness X

[M2-MGSE-REQ-1360]

Temperature X

[M2-MGSE-REQ-1370]

Humidity X

[M2-MGSE-REQ-1380]

Pressure X

[M2-MGSE-REQ-1390]

Transport environment Cleanliness X

[M2-MGSE-REQ-1400]

Load Factors (or Quasi-static Accelerations)

X X X X X X X

[M2-MGSE-REQ-1410]

Sinusoidal Accelerations X

[M2-MGSE-REQ-1420]

Random Accelerations X

[M2-MGSE-REQ-1430]

Shock Input X

[M2-MGSE-REQ-1440]

Drop Input X

REFERENCE : DATE :


ISSUE : 01 PAGE : 96/101





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[M2-MGSE-REQ-1450]

EU Safety Standard Rules X X X X X X X

[M2-MGSE-REQ-1460]

Failure Consequence Severity X X X X X X X

[M2-MGSE-REQ-1470]

Failure Tolerance X X X X X X X

[M2-MGSE-REQ-1480]

Redundancy Protection X

[M2-MGSE-REQ-1490]

Design and Proof Safety Factors X X X X X X X

[M2-MGSE-REQ-1500]

Suitable Guards

[M2-MGSE-REQ-1510]

Touch Temperature Design

[M2-MGSE-REQ-1520]

Protrusion X X X X X X X

[M2-MGSE-REQ-1530]

Indices X X X X X X

[M2-MGSE-REQ-1540]

Alignment Marks X X X X X X X

[M2-MGSE-REQ-1550]

Mechanical Stop X X

[M2-MGSE-REQ-1560]

Safe Working Load Display X X X X X X X

[M2-MGSE-REQ-1570]

Unintentional Movements X X X X X

[M2-MGSE-REQ-1580]

Sharp Edges and Corners X X X X X X X X

[M2-MGSE-REQ-1590]

Clearances X X X

[M2-MGSE-REQ-1600]

Human Engineering Criteria X X X X X X X

[M2-MGSE-REQ-1610]

I/F Accessibility X X X X X X X

[M2-MGSE-REQ-1620]

Hand Limit Weight X X X X X X X

[M2-MGSE-REQ-1630]

Hand Operation Limit Force X X X

[M2-MGSE-REQ-1640]

Sling & Lifting Accessories Provisions

X X X X X X X

[M2-MGSE-REQ-1650]

Warning Placards

[M2-MGSE-REQ-1660]

Indicators & Control Labels

[M2-MGSE-REQ-1670]

Potential Hazard Prevention

[M2-MGSE-REQ-1680]

Hazard Prevention by Design Improvement

REFERENCE : DATE :


ISSUE : 01 PAGE : 97/101





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[M2-MGSE-REQ-1690]

Warning Labels for Command/Control

[M2-MGSE-REQ-1700]

Display and Control Location

[M2-MGSE-REQ-1710]

Instruction Labels Readability

[M2-MGSE-REQ-1720]

Alarm/Emergency Indicators

[M2-MGSE-REQ-1730]

Equipment Control Position

[M2-MGSE-REQ-1740]

Control/Display Association

[M2-MGSE-REQ-1750]

Control/Display Adjustment

[M2-MGSE-REQ-1760]

Emergency Control

[M2-MGSE-REQ-1770]

Display Scales

[M2-MGSE-REQ-1780]

Marking Language

[M2-MGSE-REQ-1790]

Weight/CoG Identification X X X X X X X

[M2-MGSE-REQ-1800]

Hoisting Point Identification X X X X X X X

[M2-MGSE-REQ-1810]

Hoisting Device Reassembly X X

[M2-MGSE-REQ-1820]

Prevent Contamination ISO 8 X X X X X X X X

[M2-MGSE-REQ-1830]

Prevent Contamination ISO 7 HC X X X X X X X X

[M2-MGSE-REQ-1840]

Prevent Contamination ISO 3 AMC-9 X X X

[M2-MGSE-REQ-1850]

MGSE General Cleanliness Level X X X X X

[M2-MGSE-REQ-1860]

Cleanliness Certification X X X X X X X X

[M2-MGSE-REQ-1870]

MGSE Design for Cleanability

X X X X X X X X

[M2-MGSE-REQ-1880]

MGSE Design Oriented to Preservation of Flight H/W Ultracleanliness

X X X

[M2-MGSE-REQ-1890]

GSE Contamination Level

[M2-MGSE-REQ-1900]

Material and Processes Cleanliness Requirements

X X X X X X X X

[M2-MGSE-REQ-1910]

MGSE UltraCleaning for ISO 3/AMC-9 Environment

X X X

[M2-MGSE-REQ-1920]

MGSE Design for Ultracleaning X X X

[M2-MGSE-REQ-1930]

Acceptance Testing X X X X X X X

REFERENCE : DATE :


ISSUE : 01 PAGE : 98/101





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[M2-MGSE-REQ-1940]

Test Procedure X X X X X X X

[M2-MGSE-REQ-1950]

Test Conditions X X X X X X X

[M2-MGSE-REQ-1960]

Test Report X X X X X X X

[M2-MGSE-REQ-1970]

Dimensional and Fit Check X X X X X X X

[M2-MGSE-REQ-1980]

MGSE Mass and CoG Determination X X X X X X X

[M2-MGSE-REQ-1990]

Non Destructive Inspection X X X X X X X

[M2-MGSE-REQ-2000]

Static Load Test X X X X X X X

[M2-MGSE-REQ-2010]

Functional/Performance Test X X X X X X X

[M2-MGSE-REQ-2020]

EMC Tests (as applicable)

[M2-MGSE-REQ-2030]

Electrical Bonding Test X X X X X X X

[M2-MGSE-REQ-2040]

Leak Test X

[M2-MGSE-REQ-2050]

Drop Test X

[M2-MGSE-REQ-2060]

Documentation Language X X X X X X X X

[M2-MGSE-REQ-2070]

Supplied Documentation X X X X X X X X

[M2-MGSE-REQ-2080]

Document Format X X X X X X X X

[M2-MGSE-REQ-2090]

MGSE Shipping & Reusable Cont. X X X X X X

[M2-MGSE-REQ-2100]

Commercial Containers X X X X X X

[M2-MGSE-REQ-2110]

Storage Periods X X X X X X

[M2-MGSE-REQ-2120]

Wooden Containers X X X X X X

[M2-MGSE-REQ-2130]

Shipping Cont. Manufact. Material X X X X X X

[M2-MGSE-REQ-2140]

Packing Materials X X X X X X

[M2-MGSE-REQ-2150]

Packing Cleanliness Capability X X X X X X

[M2-MGSE-REQ-2160]

Containers Colour X X X X X X

[M2-MGSE-REQ-2170]

Protection X X X X X X

[M2-MGSE-REQ-2180]

MGSE Internal Locking X X X X X X

[M2-MGSE-REQ-2190]

Tie-down Provisions X X X X X X

REFERENCE : DATE :


ISSUE : 01 PAGE : 99/101





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[M2-MGSE-REQ-2200]

Protective Covers X X X X X X

[M2-MGSE-REQ-2210]

Waterproof Capability X X X X X X

[M2-MGSE-REQ-2220]

Desiccant Salts X X X X X X

[M2-MGSE-REQ-2230]

Handling Provisions X X X X X X

[M2-MGSE-REQ-2240]

Cover Lid Handling Provisions X X X X X X

[M2-MGSE-REQ-2250]

Containers Handles X X X X X X

[M2-MGSE-REQ-2260]

Containers Closing and Opening Devices

X X X X X X

[M2-MGSE-REQ-2270]

Containers Shock Indicator X X X X X X

[M2-MGSE-REQ-2280]

Containers Dimensions X X X X X X

[M2-MGSE-REQ-2290]

Un-packaging Tools X X X X X X

[M2-MGSE-REQ-2300]

Transport Container Marking X X X X X X

[M2-MGSE-REQ-2310]

Contract X X X X X X

[M2-MGSE-REQ-2320]

Container Label Position X X X X X X

[M2-MGSE-REQ-2330]

Container Annexed Documentation

X X X X X X X

[M2-PP-REQ-0010] Subco Operators Training by P-PPE

X X X X X X X X

[M2-PP-REQ-0020] MGSE Compatibility with IPA Wiping

X X X X X X X X

[M2-PP-REQ-0030] MGSE Design Accessible to IPA Wiping

X X X X X X X X

[M2-PP-REQ-0040] MGSE Compatibility with Bioburden Assays

X X X X X X X X

[M2-PP-REQ-0050] MGSE Design Accessible to Assays

X X X X X X X X

[M2-PP-REQ-0060] MGSE Material List and Relevant Data Sheets

X X X X X X X X

[M2-PP-REQ-0070] Fluids in contact with MGSE [M2-PP-REQ-0080] MGSE Cleaning before Delivery to

TASI X X X X X X X X

[M2-PP-REQ-0090] Subco Operators Training by P-PPE

X X X X

[M2-PP-REQ-0100] MGSE Compatibility with IPA Wiping

X X X X

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[M2-PP-REQ-0110]

MGSE Design Accessible to IPA Wiping X X X X

[M2-PP-REQ-0120]

MGSE Compatibility with Bioburden Assays

X X X X

[M2-PP-REQ-0130]

MGSE Design Accessible to Assays X X X X

[M2-PP-REQ-0140] MGSE Material List and Relevant Data Sheets

X X X X

[M2-PP-REQ-0150]

Fluids in contact with MGSE

[M2-PP-REQ-0160] MGSE Cleaning before Delivery to TASI

X X X X

[M2-PP-REQ-0170] MGSE Compatibility with Sterilization Process DHMR

X X X X

[M2-PP-REQ-0180] MGSE DHMR Cycles X X X X

[M2-PP-REQ-0190] MGSE Limit Dimensions X X X X

REFERENCE : DATE :


ISSUE : 01 PAGE : 101/101




END OF DOCUMENT