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Preliminary Design of Low-Thrust Interplanetary MissionsFor interplanetary missions, highly efficient electric propulsion systems can be used to increase the mass delivered to the destination and/or reduce the trip time over typical chemical propulsion systems.
Document ID
20210002768
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
hdl:2014/16916
Authors
Flanagan, S.
Sims, J.
Date Acquired
August 16, 1999
Publication Date
August 16, 1999
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
interplanetary
missions
electric
propulsion
Deep
Space
1
New
Millenium
Program

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