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Hydrazine monopropellant provides 0.5-600 lb thrustHydrazine monopropellant performance and characteristics, describing various catalysts and propulsion systems
Document ID
19700036149
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Price, T. W.
Date Acquired
August 5, 2013
Publication Date
October 1, 1969
Publication Information
Publication: SPACE(AERONAUTICS, VOL. 52, P. 70-72.
Subject Category
Propellants
Accession Number
70A12265
Distribution Limits
Public
Copyright
Other

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