Application Specific Actuation Systems (ASAS) · - Petrol cap door opening actuator (automotive) SMARQ MATERIAL CHARACTERIZATION ITI Assessment on smart materials (SMARQ) for space

2017 © 2016 ARQUIMEA Enterprises S.L. – All rights reserved www.arquimea.com

http://www.arquimea.com/

© 2016 ARQUIMEA Enterprises S.L. – All rights reserved www.arquimea.com

HI-REL COMPONENTS

AEROSPACE

ONBOARD SYSTEMS

DEFENCE & SECURITY BIOTECHNOLOGY

Headquarters

Madrid (ES)

Branches & Subsidiaries

Frankfurt Oder (DE)

Hong Kong (CN)

Shareholder

Diego Fernández, PhD.

13M€ revenues in FY16

2M€ EBITDA

Employees 70

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TECHNOLOGY

INVESTMENT

our mission

to deliver useful technology everywhere





MAIN COSTUMERS & PARTNERS

TECHNOLOGIES

- SPACE MICROELECTRONICS & ELECTRONICS

- SPACE ACTUATORS & MECHANISMS

- NUCLEAR WASTE DISPOSAL TECHNOLOGIES

COMPANY OVERVIEW

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MEMBER OF

Supplier of Hi-Rel technologies Strong R&D activity and product-oriented strategy

SPACE & HI-REL PRODUCTS

ITAR FREE



SPACE ELECTRONICS & µELECTRONICS

RAD-HARD IC DESIGN

ANALOG, DIGITAL, MIXED-SIGNAL

ELECTRICAL & RADIATION CHARACTERIZATION

RAD-HARD IPS & LIBRARIES

ASICS / FPGAS / STANDARD PARTS

ELECTRONIC SYSTEMS

LOW POWER / HI-REL APPLICATIONS

SPACE R&D

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MICROELECTRONICS Supply Chain, Capabilities & Alliances

DESIGN FLOW CAPABILITIES PARTNERS

DEFINITION &

FEASIBILITY ANALYSIS

Spec review

Technology selection

ASIC development plan

DESIGN

Rad-hard IPs and ICs

Rad-hard smart power

Test vehicles

Technology hardening by design and modeling

Space FPGAs

FPGA to ASIC conversion

ESD protections

Sofics

DESIGN VERIFICATION

Functional

Reliability

Radiation simulation

MANUFACTURING

MPW

MLM

Full mask

IHP (SGB25RH, SG13RH)

ON SEMI (I3T80)

UMC 180nm / DARE (IMEC)

Atmel (ATMX150RHA)

ASSEMBLY Package selection

Package design

HCM

MICROSS

VALIDATION

Qualification according to ESCC

Screening

Mechanical, Electrical and ESD test

Reliability test

Radiation test (SEE, SEL, TID)

SERMA

MICROSS

5 © 2017 ARQUIMEA Enterprises S.L. – All rights reserved www.arquimea.com




SPACE MICROELECTRONICS Main Projects

ASICs & FPGAS CUSTOMER

REDSAT ASIC set ELSA

Smart Power Chip Set for reconfigurable antenna control. Qualified for Small GEO Satellite.

1500+ flight units delivered since 2012

Airbus Defence & Space

600 ASICS ALREADY IN ORBIT

COSMIC VISION reconfigurable mixed-signal ASICs (MF and HF) European Space Agency – ESA

Avionics mixed-signal ASIC for low-cost satellites (analog IPs design) IHP Microelectronics

SWIPE ASIC for Radiometry EU (FP7)

Design and integration of a RH ADC IP for an Scalable Sensor Data Processor ASIC (SSDP) Thales Alenia Space (ESA project)

QUANTUM – Fast Beam Hopping Enabled Digital ASIC Airbus Defence & Space

TMTC ASIC – Mixed-signal ASIC for telemetry and telecommand European Space Agency – ESA

QUANTUM – Space FPGA’s implementation and verification Airbus Defence & Space

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STANDARD COMPONENTS CUSTOMER

RAD-HARD Octal 500 Mbps Bus LVDS Repeater; LVDS driver; LVDS receiver ESA – European Components Initiative

SEPHY – 10/100Mbps Space Ethernet Physical Layer Transceiver European Commission – H2020

RAD-HARD IPs & TECHNOLOGY CHARACTERIZATION CUSTOMER

IHP 250 nm rad-hard mixed-signal library R&D project (Eurostars)

ON SEMI 0.35 µm rad-hard mixed-signal library R&D project (ILB programme)

UMC 180 nm analog IP cores Internal R&D project

Electrical and radiation characterization of IHP SGB25RH and SG13RH technologies IHP Microelectronics



SPACE ACTUATORS & MECHANISMS

NON-EXPLOSIVE, LOW-SHOCK, RESETTABLE

HDRM, PIN PULLER, LINEAR & ROTARY, VALVES

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SMA ARTIFICIAL MUSCLES TECHNOLOGY

SMARQ® HIGH TEMPERATURE SHAPE

MEMORY ALLOYS (SMA)



SPACE ACTUATORS SMARQ actuators roadmap

R&D / CUSTOM DEVELOPMENTS

- Dust sensor cleaning (for Mars)

- Prototype / BB / EQM

- Petrol cap door opening actuator (automotive)

SMARQ MATERIAL CHARACTERIZATION

ITI

Assessment on smart materials (SMARQ) for space mechanisms

- HDRM

- Pin puller

- Rotary actuators

GSTP/ARTES

Pin puller and HDRM family qualification to TRL6

OFF-THE-SHELF PRODUCTS

In-orbit validation. Flight missions (JUICE, METOP, PROBA 3…)

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SPACE ACTUATORS Off-the-shelf HDRAs

• Low-shock, non-explosive

• Operation temperature

• Standard temperature version (up to +70ºC)

• Extended temperature version (up to +120oC

• Redundant SMA trigger (two independent initiators)

• Resettable by end user (manual reset)

• COTS and custom configurations available

• Version 1 Qualified to TRL6 according to ECSS

• Version 2 Qualification to TRL9 ongoing

HDRA ARQ.REAC.S02.053 ARQ.REAC.S02.153 ARQ.REAC.S02.353

Hold-Down Load [N] 5,000 15,000 35,000

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SPACE ACTUATORS Off-the-shelf Pin Pullers

PIN PULLER ARQ.PPLL.S01.250 ARQ.PPLL.S01.051 ARQ.PPLL.S01.012 ARQ.PPLL.S02.052

Pull Force (min) [N] 25 50 100 500

• Low-shock, non-explosive

• Operation temperature

• Standard temperature version (up to +70ºC)

• Extended temperature version (up to +120oC

• Redundant SMA trigger (two independent initiators)

• Resettable by end user (manual reset)

• COTS and custom configurations available

• Version 1 Qualified to TRL6 according to ECSS

• Version 2 to be qualified expectes Q3/Q4 2018

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SPACE ACTUATORS Main PROJECTS

YEAR PROJECT CUSTOMER DESCRIPTION COMMENTS

2010 ITI ESA Validation of SMARQ (ARQ‐I’s own proprietary Shape Memory Alloy) technology for space applications.

2010 GSTP ESA Design, development and qualification of two European pin pullers (50N and 100N) for extended temperature operation range.

2011 Confidential Delivery of 1 EQM unit of pin puller 500N standard temperature device.

2012 Confidential Delivery of 5 FM units of pin puller 500N standard temperature device.

No information about the flight mission

2014 JUICE SERENUM Delivery of 1 EQM unit of the REACT 15KN version 1 extended temperature range for JUICE magnetometer experiment

No flight model requested so far

2014 MetOP II KDA Delivery of 1 EQM unit of the REACT 2.5KN version 1 extended temperature range

No flight model requested so far

2015 CAST Delivery of 1 EQM unit of REACT 2.5KN version 1 extended temperature range for picosat launcher.

No flight model was requested

2016 CAST Design, development and qualification of HDRM & Deployment hinges .

FM delivery planned for Nov 2017

2016 Μhetsat SITAEL Design, development and qualification of HDRM & Deployment hinges .

FM delivery planned for Dec 2017

2017 E-SAIL LUXSPACE Design, development and qualification of HDRM FM delivery planned for Dec 2017

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MetNet Precursor Mission

In-flight calibration system based on a reflector stick inserted in the

optical path by means of a novel rotary actuator based on a

proprietary Shape Memory Alloy.

• Mass: 41.2 g

• Main dimensions: 85x65x20 mm

• Operational temperature range: -90 to +25oC

• Nominal Power Consumption: 360 mW

FLIGHT MODEL DELIVERED

IR system Rotary actuator

SMA

Active measurement using back scattering to estimate the concentration of particles in the airborne dust.

SPACE R&D

Rotary actuator for Space Science

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Space Wireless sensor networks for Planetary Exploration

Smart technology for artificial muscle applications in Space

10/100Mbps Space Ethernet Physical Layer Transceiver

Resettable Hold-Down and Release Actuator (In-Orbit Validation)

LIBRA Development of a space-qualified rad-hard library (IHP SGB25RH)

PISA Power robust IC design for space applications

Main R&D European projects

Precision-Based Drive Mechanisms for High Precision Energy-Efficient

Positioning devices. SME instrument PHiDRIVE

SQS Automated seminal quality platform for swine reproduction upgrade.

SME instrument ZOITECH LABS

EXQUDO (Civil explosives e-traceability and e-documentation management system)

EC/ ISEC

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MICACT Marie Sklodowska Curie Innovative Training Networks. Electroactive

polimers (EAP) actuators

SECHIS SERDES for space applications


Ferran Tejada CEO – Arquimea Deutschland GmbH

[email protected]

+49 (0) 173 618 1828

www.arquimea.com

ARQUIMEA INGENIERÍA, SLU c/ Margarita Salas 10, 28919 Leganés (Madrid) – ES

Tel.: +34 91 689 80 94 / [email protected]

ARQUIMEA DEUTSCHLAND GmbH Im Technologiepark 1, 15236 Frankfurt (Oder) – DE

Tel.: +49 335 557 1717 / [email protected]

Francisco Gutiérrez CEO – Arquimea Ingeniería S.L.U.

[email protected]

+34 627 495 410

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mailto:[email protected]





Documents

Application Specific Actuation Systems (ASAS) · - Petrol cap door opening actuator (automotive) SMARQ MATERIAL CHARACTERIZATION ITI Assessment on smart materials (SMARQ) for space