European EPPM suppliers (pdf) - ESA
European EPPM suppliers (pdf) - ESA
European EPPM suppliers (pdf) - ESA
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Name of the<br />
item<br />
EPMEC<br />
RUAG Zurich<br />
TROM<br />
RUAG Zurich<br />
MTOM<br />
RUAG Zurich<br />
ITAM<br />
RUAG Austria<br />
TPM<br />
RUAG Austria<br />
<strong>European</strong> <strong>EPPM</strong> <strong>suppliers</strong><br />
Maturity<br />
Technical Characteristics Status<br />
(TRL)<br />
Applicability to Missions<br />
Pointing range:<br />
TRL 9 Smart 1 (3 years operation)<br />
- 9.5 half cone<br />
Science missions<br />
Mass : 10 Kg<br />
Deep space missions<br />
Payload : 1 x PPS1350<br />
Main engine<br />
Life time: 4 years storage<br />
3 years in orbit<br />
Low Power Electric Thrusters<br />
Pointing range:<br />
- Axis 1: 90<br />
- Axis 2: 35<br />
- Axis 3: -5 to 95<br />
- Axis 4: 0 to 180one shot<br />
Mass: 22.9 Kg<br />
Payload: 2 x PPS1350<br />
Life time: 4 years storage<br />
15 years in orbit<br />
Pointing range:<br />
- Axis 1: 35<br />
- Axis 2: 15<br />
Mass: 18 Kg<br />
Payload: 2 x PPS1350<br />
Life time: 4 years storage<br />
15 years in orbit<br />
Pointing range:<br />
- 6 half cone<br />
Mass: 4.3Kg<br />
Payload:<br />
- 1 x RIT10 and,<br />
- 1 x T5.<br />
Life time: 5 years storage<br />
15 years in orbit<br />
Pointing range:<br />
- 6.5 half cone<br />
Mass: 10.7Kg<br />
Payload:<br />
- 2 x PPS1350 or<br />
- 2 x SPT10 or<br />
- 2 x ROS2000 or<br />
- Any combinations<br />
Life time: 5 years storage<br />
15 years in orbit<br />
TRL 3 Tailored to ConeXpress / Orbit<br />
Life Extension Vehicle<br />
Extended pointing range<br />
capabilities<br />
Full electric Spacecraft<br />
Low Power Electric Thrusters<br />
Development stopped.<br />
TRL3 Smart Olev<br />
Orbit Life Extension Vehicle<br />
Science missions<br />
Deep space missions<br />
Main engine, NSSK and wheel<br />
off loading<br />
Low Power Electric Thrusters<br />
Under development<br />
TRL9 Telecom platforms<br />
Artemis<br />
Low Power Electric Thrusters<br />
NSSK and orbit raising (not<br />
nominal)<br />
TRL7 Telecom platforms<br />
Eurostar 3000 LX<br />
Qualified as part of the ATMA<br />
in collaboration with EADS<br />
Astrium (FR and UK)<br />
Low Power Electric Thrusters<br />
NSSK and wheel off loading<br />
Qualified at Thruster Module<br />
level<br />
FM procurement pending
TPA<br />
RUAG Austria<br />
<strong>EPPM</strong><br />
RUAG Austria<br />
<strong>EPPM</strong><br />
RUAG Austria<br />
TOM<br />
RUAG Austria<br />
TOM<br />
Thales Alenia<br />
Space - Cannes<br />
Pointing range:<br />
- Axis 1: + 21.09 / - 7.85<br />
- Axis 2: + 21.09 / - 7.85<br />
Mass: 10 Kg<br />
Payload: 1 x T6<br />
Life time: 7 years storage<br />
6.6 years in orbit<br />
Pointing range:<br />
- Axis 1:<br />
- Deployment : 0 / +120<br />
- Pointing: 15<br />
- Axis 2: 15<br />
Mass: 12 Kg<br />
Payload:<br />
- 1 x T6 or<br />
- 1 x RIT22 or<br />
- 1 x PPS 5000<br />
Life time: 6.5 years storage<br />
16 years in orbit<br />
Pointing range:<br />
- Axis 1:<br />
- 0 / +90<br />
- 15<br />
- Axis 2: 15<br />
Mass: 16 Kg<br />
Payload:<br />
- 2 x T6 or<br />
- 2 x RIT22 or<br />
- 2 x PPS 5000 or<br />
- Any combinations.<br />
Life time: 6.5 years storage<br />
16 years in orbit<br />
Pointing range:<br />
- Axis 1: 45 mm<br />
- Axis 2: 60 mm<br />
- Axis 3: 180 <br />
- Axis 4: 30 one shot<br />
Mass: 20 Kg<br />
Payload: 2 x PPS 1350<br />
Life time: 5 years storage<br />
16 years in orbit<br />
Pointing range:<br />
- 8 half cone<br />
Pointing accuracy: 0.01<br />
TRL3 BepiColombo<br />
Science missions<br />
Deep space missions<br />
Main engine<br />
High Power Electric Thrusters<br />
Under development<br />
TRL4 Future high power telecom<br />
platforms<br />
Extended pointing range<br />
capabilities<br />
High Power Electric Thrusters<br />
Under development<br />
Full electric Spacecraft<br />
T6 requirement for axis 1<br />
deployment is 0 / +90<br />
TRL3 Future high power telecom<br />
platforms<br />
High Power Electric Thrusters<br />
Orbit raising, NSSK and wheel<br />
off loading<br />
Development stopped<br />
TRL3 Tailored to CX2<br />
Small telecommunication<br />
platforms<br />
Low Power Electric Thrusters<br />
Under development<br />
Full electric Spacecraft<br />
TRL 8 Telecommunication platforms<br />
Stentor<br />
Astra 1K
TOM<br />
Thales Alenia<br />
Space - Cannes<br />
TOM<br />
Thales Alenia<br />
Space - Cannes<br />
Mass:12 Kg<br />
Payload:<br />
- 1 x PPS1350 and<br />
- 1 x SPT100<br />
Life time: 5 years storage<br />
15 years in orbit<br />
Duty cycle: 38x10 6 motor<br />
steps<br />
Pointing range:<br />
- 8 half cone<br />
Pointing accuracy: 0.01<br />
Mass:12 Kg<br />
Payload: 2 x SPT100<br />
Life time: 5 years storage<br />
15 years in orbit<br />
Duty cycle: 38x10 6 motor<br />
steps<br />
Pointing range:<br />
- 8 half cone<br />
Pointing accuracy: 0.01<br />
Mass:14 Kg<br />
Payload: 2 x PPS1350<br />
Life time: 5 years storage<br />
15 years in orbit<br />
Duty cycle: 38x10 6 motor<br />
steps<br />
SpaceBus 4000 platform<br />
Low Power Electric Thrusters<br />
Demonstrator<br />
Failure of the launchers<br />
TRL 9 Telecommunication platforms<br />
Eurostar 3000 platform<br />
SpaceBus 4000 platform<br />
Low Power Electric Thrusters<br />
NSSK and wheel off loading<br />
TRL 5 Telecommunication platforms<br />
Eurostar 3000 platform<br />
SpaceBus 4000 platform<br />
AlphaBus / AlphaSat<br />
Low Power Electric Thrusters<br />
NSSK and wheel off loading<br />
Under qualification for<br />
AlphaSat (early 2010)<br />
FMs for AlphaSat under<br />
integration.
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