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Propulsion system selection considerations for the Voyager spacecraft.Propulsion system selection considerations for Voyager spacecraft including Minuteman solid with liquid restartable midcourse, orbit trim system, LEM descent stage and transtage
Document ID
19670033567
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Benson, R. A.
Date Acquired
August 3, 2013
Publication Date
November 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 66-974
Report Number: AIAA PAPER 66-974
Accession Number
67A12296
Funding Number(s)
CONTRACT_GRANT: JPL-951113
Distribution Limits
Public
Copyright
Other
Keywords
SPACECRAFT PROPULSION
PROPULSION SYSTEM
VOYAGER PROJECT
SPACECRAFT DESIGN

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