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Hypergolic control fluid effects on the combustion of solid propellants.Solid propellants combustion characteristics under hypergolic fluid injection control conditions including burning rate, vacuum ignition, low pressure stability, etc
Document ID
19680036544
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Coates, R. L.
Cohen, N. S.
Roberts, R. W.
Date Acquired
August 4, 2013
Publication Date
January 1, 1968
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS.
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 68-94
Report Number: AIAA PAPER 68-94
Meeting Information
Meeting: AEROSPACE SCIENCES MEETING
Location: NEW YORK, NY
Start Date: January 22, 1968
End Date: January 24, 1968
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
68A17516
Funding Number(s)
CONTRACT_GRANT: NAS7-444
Distribution Limits
Public
Copyright
Other

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