Genesis extended mission trajectory design

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This paper will discuss the design of the various trajectory options for some of these proposed extended missions.

Document ID

20210001724

Acquisition Source

Jet Propulsion Laboratory

Document Type

Preprint (Draft being sent to journal)

External Source(s)

Authors

Date Acquired

January 1, 2005

Publication Date

January 1, 2005

Publication Information

Publisher: Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2005.

Distribution Limits

Public

Other

Technical Review

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