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European Space Propulsion www.espdeltav.co.uk
Leading the Way to Electric Propulsion in Belfast
February 2014
1
Overview
• Strategic New Entrant To European Space Industry
• Provide Aerojet Rocketdyne Heritage In-Space Propulsion Based in Belfast, UK
• Wholly Owned Subsidiary of Aerojet Rocketdyne, Inc.
• Manufactured by Europeans and Supported By A Lower Cost Supply Chain
• UK Registered
A Lower Cost, High Quality Propulsion Supplier
For The European Market
2
European Space Propulsion A New European Propulsion Company
Products / Services
• N2H4 System Integration & Assembly
• Select N2H4 Thruster Manufacturing
• Electric Propulsion Thrusters/Systems
• Green Propulsion Development
• In-Space Chemical Propulsion Testing
• Satellite Fueling Services
Business Strategy
• Stepwise Implementation Systems, Select
Thrusters, Testing
• Selected Teammate/Site With Maximum
Capability Strategy
• Rigorous Training and Validation Program
European Space Propulsion Ltd. Formed In July 2012
3
Site and Teammate Selection - UK Thales Air Defense Ltd. (TADL), Belfast
• Description
• Formerly Shorts Missile Systems
• 500 Employees, £80M Turnover
• Missile Manufacturing & Test
• Benefit To ESP
• Large Clean Room Assembly Areas
• State Of Art Machine Shop (35% Out Of House)
• N2H4 Use Both Storage & Test
• Available Skilled Workforce
• TADL Has Significant Experience in
Technology Transfer
Castlereagh, Belfast
(Manufacturing & Assembly)
Crossgar
(N2H4 Testing)
4
ESP – TADL – Aerojet Rocketdyne – A Powerful Force in Space
Propulsion in Europe
ESP Controlled
Provided and
Operated by TADL (Subcontract)
ESP Controlled
Provided and
Operated by TADL (Subcontract)
European Space Propulsion Site /
Facility Usage
Crossgar
30
m
30
m
Production Area
N2H4 Test Facility
ESP Headquarters
(Castelreagh)
Northern Ireland
Belfast
Castlereagh
5
EO-1 System ARCM System Atlas II Roll Control Module
Flight Proven Propulsion Products
• Monopropellant Thrusters
• Licensed MR-103 Engine and 4 –N MR-111 Engine
• Fully Integrated Monopropellant Propulsion Systems
• Leverages Aerojet Rocketdyne’s Flight Heritage With
Designing and Fabricating > 230 Propulsion Systems
• Electric Propulsion
• Transfer heritage XR-5 and ESP development of Euro-4000
Hall Thruster
• Green Propellant
• Leveraging Aerojet Rocketdyne’s Work With AF-M315E which
Offers Lower Toxicity and Higher Density-Isp Performance
Than Hydrazine
Hall Thruster
MR-111
MR-103
6
Aerojet Rocketdyne Electric Propulsion
• Aerojet Rocketdyne has been developing and delivering Electric
Propulsion thrusters and systems since 1984
• Industry Leader in Electric Propulsion Systems
• Full spectrum of EP technologies: Electrothermal, Arcjet,
Electromagnetic, Hall Effect and Gridded Ion
• All capabilities and facilities for design, analysis, manufacture
and test of complete EP systems
• 8 flight qualified power processor designs
• Over 150 shipsets with 500 thrusters flown
Aerojet Rocketdyne is committed to providing electric
propulsion solutions across the range of applications
AEHF Star-2 Intelsat 23 Kizuna A2100™ ACeS ARGOS
7
Electrothermal
Hydrazine Thruster
Hydrazine Arcjets
and Power Processing Unit
High Power Ammonia
Arcjet and Feed System
Pulsed Plasma Thruster Hall Thruster Firing Xenon Ion Engine
2011-H-4231
Approved for Public Release and Export
8
AR Electric Propulsion Heritage
Aerojet Rocketdyne has delivered over 500 electric propulsion devices.
2010 – Highest Power, Highest
Efficiency Hall System Ever
Flown
Advanced EHF
Aerojet Electric Propulsion Heritage
1983 – First Flight of Electrothermal Hydrazine
Thruster (EHT)
RCA Astro
1991 – First Flight of Improved
Electrothermal Hydrazine Thruster
(IMPEHT)
Flying on 131 satellites
1993 – First Flight of Hydrazine
Arcjet System
Telstar 4
1998 – First Flight of Hall
Thruster System on Western
Spacecraft
STEX
1999 – Highest Power EP
Device Flown
30 kW Ammonia Arcjet System
ARGOS/ESEX
2002 – First All Propulsive ACS –
Pulsed Plasma Thruster (PPT)
System
Earth Observing - 1 1996 – First Flight of 2 kW Hydrazine
Arcjet System
Flying on 41 satellites
Aerojet has been a leader in
the implementation of
Electric Propulsion
9
2013 – Three AEHF SVs Now
Delivered to GEO
Advanced EHF
Aerojet Hall Effect Propulsion
• XR-5 Hall Thruster Propulsion System
• One thruster per PPU in each string
• 5 kW total input power per thruster at 70 V
• 280 mN per thruster at 1815 sec, Xenon
• 3 shipsets flown; 3 more on contract
• XR-12 and XR-20 High Power Hall Thrusters
• One thruster per PPU in each string
• Thruster input power:12 kW (XR-12), up to 20 kW (XR-20)
• 780 mN per thruster at 2300 sec, Xenon (XR-12)
• XR-12 developed for TSAT, XR-20 in development for AFRL
BPT-4000 Hall Thruster
Propulsion System
XR-12 Thruster, Cathode and
Power Processing Unit
11
XR-5 Hall System
• Multi-mode 4.5 kW class Hall thruster system designed
for military and commercial GEO satellite applications
• Single string architecture
• Baseline system qualification testing completed in
2005
• First flight on Advanced EHF satellite launched August
2010
• Full GTO to GEO orbit transfer completed October,
2011 on AEHF SV1 with BPT-4000 system
• SV2 and SV3 flown with ~50% GTO-GEO EPOR
• 12 thruster strings flown; 12 currently in production
12
XR-5 Hall Thruster
2012-H-4248 13
2 kW 3 kW 4.5 kW
Thrust (300 Volts) 133mN 190mN 277mN
Thrust(400 Volts) 117mN 173mN 256mN
Specific Impulse (300 V) 1606s 1727s 1838s
Specific Impulse (400 V) 1770 s 1905 s 2050s
Multi Mode Operation:
• High Thrust: 300V at 4.5 kW • High Isp: 400V at 3 or 4.5 kW
Cathode based on NASA’s ISS plasma contactor
Demonstrated Thruster Life Capability >10,000 hours and >7000
cycles
XR-5 Key Discriminators
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Key Discriminating Advantage Benefit to Users
Only Flight Proven 5kW Hall Thruster Lowest technical and schedule risk
Highest Performance Hall Thruster Shortest orbit raising duration and
lowest propellant mass, providing
highest financial return
Longest demonstrated life of any Hall
Thruster
Enables full GTO-GEO EPOR; and
potentially full LEO-GEO EPOR
All system integration issues resolved
and validated
Lowest technical risk
Broadest operating range of any Hall
Thruster
Enables broad mission application and
mission flexibility
Enhanced affordability Improved financial return
Euro-4000 Overview
• ESP proposes to provide for sales in the EU, a European version of the Aerojet Rocketdyne XR-5 (BPT-4000) Hall Thruster and XFC
• New ESP thruster will be designated the Euro-4000
• Intent of this new Euro-4000 is to:
• Retain heritage design/processes for elements that are critical to flight/qualification heritage
• Incorporate European market required design features and European suppliers for elements that do not impact qual life
• Drive lowest cost solution
ESP Plans to Introduce Euro-4000 Hall Thruster to EU Market
15
Euro-4000 Description
• Euro-4000 Thruster
• Heritage XR-5 Thruster Modified for European Market
• Maintain critical qual/flight heritage elements
• Incorporate new European designs and suppliers
• Validate with delta-qual (all qual tests, except abbreviated life test)
• Euro-4000 XFC
• All new XFC Modified For European Market
• Incorporate European designs and suppliers
• Validate thru full qualification test program
16
Heritage XR-5 Thruster
Heritage XR-5 XFC
Long Term EP Roadmap
• Immediate Offering:
• Flight Heritage XR-5 Thruster and XFC
• Within Next 2 Years:
• Euro-4000 Thruster and XFC
• Within Next 5 Years:
• Euro-4000HV (high-voltage) Thruster and XFC
• High-Isp Euro-4000 thruster coupled with externally developed high-voltage PPU
• Within 6-10 Years:
• Fully European Developed Next Generation Hall Thruster
• Targeting 10kW-class thruster
• Targeting Expanded Operating Range:
• High-Isp capability up to 3,000-sec
• High-Thrust capability up to 90mN/kW
17
Summary
• European Space Propulsion is a New Entrant to the European
Market Based in Belfast, UK Offering a Variety of Technologies
• Monopropellant Thrusters & Systems
• Green Propellants
• Electric Propulsion
• Aerojet Rocketdyne has a Long Heritage of Developing,
Qualifying and Flying Innovative Electric Propulsion Products
• XR-5 is the Only Flight Proven 5kW Hall Thruster
• European Space Propulsion has developed a Transition and
Manufacturing Plan for the Euro-4000
• Draws heavily from the flight proven XR-5 (BPT-4000)
18