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propulsion system
Standard
ECSS-E-ST-35C Rev. 1Definition
system to provide thrustNotes
- NOTE 1 In this standard it is also referred to as the system
- NOTE 2 Propulsion system comprises all components used in the fulfilment of a mission, e.g. thrusters, propellants, valves, filters, pyrotechnic devices, pressurization subsystems, feeding system, tanks and electrical components.
- NOTE 3 Electrical power sources are only included in Electrical propulsion system.
Relations
- ECSS-E-ST-35C Rev. 1 — burning time, tb
- ECSS-E-ST-35C Rev. 1 — contaminant
- ECSS-E-ST-35-10C — contaminant gas
- ECSS-E-ST-35C Rev. 1 — end of flight or final mass
- ECSS-E-ST-35C Rev. 1 — envelope
- ECSS-E-ST-35C Rev. 1 — ground support equipment GSE
- ECSS-E-ST-35C Rev. 1 — initial mass
- ECSS-E-ST-20-06C Rev.1 — ion engine
- ECSS-E-ST-35C Rev. 1 — loaded mass
- ECSS-E-ST-35-03C — LPS
- ECSS-E-ST-35C Rev. 1 — residual mass
- ECSS-E-ST-35C Rev. 1 — system
- ECSS-S-ST-00-01C — system
- ECSS-E-ST-35C Rev. 1 — thrust
- ECSS-E-ST-35C Rev. 1 — total impulse
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