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Fluorine-Hydrazine Propulsion Technology updateThe current status of the fluorine hydrazine propulsion system development is discussed. Progress on the components, rocket engine, and system design is presented. A detailed look at a fluorine hydrazine system as a potential propulsion option for the Galileo Project (Jupiter orbiter) is delineated and the results of safety and technical reviews which were accomplished to verify the feasibility of this option are summarized.
Document ID
19800021890
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bond, D. L. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Appel, M. A. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Kruger, G. W. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1980
Publication Information
Publication: APL The 1980 JANNAF Propulsion Meeting, Vol. 5
Subject Category
Spacecraft Propulsion And Power
Accession Number
80N30391
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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