Engine performance parameter, such as thrust, efficiency, specific mass, thruster input, power, thrust-to-power ratio and discharge current have been calculated with specific impulse the indupendent variablel.
Performance Estimate of Large-Scale Ion Engines for SEI-Type Missions Using C(sub 60) Propellant
1993-01-01
Preprint
No indication
English
Manned Mars Missions using Propellant from Space
British Library Conference Proceedings | 1993
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NTIS | 2008
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