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Effect of surface reactions on the solid propellant response function.Surface coupled heat release effect on oscillatory amplitude of pressure coupled response in solid propellant
Document ID
19680038873
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Marxman, G. A.
Wooldridge, C. E.
Date Acquired
August 4, 2013
Publication Date
March 1, 1968
Publication Information
Publisher: AIAA JOURNAL, VOL. 6, P. 471-478.
Subject Category
Propellants
Meeting Information
Meeting: SOLID PROPULSION CONFERENCE
Location: ANAHEIM, CA
Country: US
Start Date: June 6, 1967
End Date: June 8, 1967
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, INTERAGENCY CHEMICAL ROCKET PROPULSION GROUP
Accession Number
68A19845
Funding Number(s)
CONTRACT_GRANT: NAS7-389
CONTRACT_GRANT: AF 49/638/-1367
Distribution Limits
Public
Copyright
Other

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