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Performance Estimate of Large-Scale Ion Engines for SEI-Type Missions Using C(sub 60) PropellantEngine 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.
Document ID
20060039366
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
External Source(s)
hdl:2014/35871
Authors
Mueller, Juergen
Date Acquired
August 23, 2013
Publication Date
January 1, 1993
Distribution Limits
Public
Copyright
Other
Keywords
Engines

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