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Advanced Liquid Propulsion SystemsAdvanced liquid propellants for spacecraft propulsion - nitrogen tetroxide and hydrazine
Document ID
19650022841
Acquisition Source
Legacy CDMS
Document Type
Other - N65-32442
Authors
R N Porter (Jet Propulsion Laboratory La Cañada Flintridge, United States)
D D Evans (Jet Propulsion Laboratory La Cañada Flintridge, United States)
W H Tyler (Jet Propulsion Laboratory La Cañada Flintridge, United States)
W F MacGlashan (Jet Propulsion Laboratory La Cañada Flintridge, United States)
O F Keller (Jet Propulsion Laboratory La Cañada Flintridge, United States)
Date Acquired
August 2, 2013
Publication Date
June 30, 1965
Publication Information
Publication: Space Programs Summary No. 37-33, Volume IV, for the Period April 1, 1965, to May 31, 1965. Supporting Research and Advanced Development
Publisher: National Aeronautics and Space Administration
Volume: IV
Subject Category
Propulsion Systems
Report/Patent Number
NO. 37-33
N65-32442
Accession Number
65N32442
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PROPULSION
NITROGEN OXIDE
HYDRAZINE
LIQUID PROPELLANT
SPACECRAFT PROPULSION
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IDRelationTitle19650022809Collected WorksSpace Programs Summary No. 37-33, Volume Iv, April 1 - May 31, 1965. Supporting Research and Advanced Development
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