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Preliminary Design of Low-Thrust Interplanetary MissionsA direct optimization method intended to be used primarily for preliminary design of low-thrust interplanetary trajectories, including those with multiple gravity assists, is presented.
Document ID
20210003001
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
hdl:2014/17923
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
trajectory
interplanetary
low-thrust
preliminary
design

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