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Propulsion subsystem design for Jupiter orbiter missionsJupiter orbiter spacecraft propulsion system design, noting advantages of fluorine/hydrazine propellant combination
Document ID
19710057228
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Don, J. P.
Phen, R. L.
Date Acquired
August 6, 2013
Publication Date
June 1, 1971
Publication Information
Publisher: AMERICAN ASTRONAUTICAL SOCIETY,
Subject Category
Propulsion Systems
Report/Patent Number
AAS PAPER 71-154
Report Number: AAS PAPER 71-154
Meeting Information
Meeting: ANNUAL MEETING ON JUPITER ORBITERS AND PROBES - A PRELIMINARY ASSESSMENT OF REQUIREMENTS
Location: SEATTLE, WA
Start Date: June 28, 1971
End Date: June 30, 1971
Sponsors: AMERICAN ASTRONAUTICAL SOCIETY
Accession Number
71A37925
Distribution Limits
Public
Copyright
Other

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