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Investigation of gaseous secondary injection thrust vector control considering primary nozzle overexpansion, frequency response, and injection anglePerformance characteristics of gaseous secondary injection thrust vector control in overexpanded primary nozzles under sea level conditions
Document ID
19680007612
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
August 4, 2013
Publication Date
January 1, 1968
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-66533
Report Number: NASA-CR-66533
Accession Number
68N17081
Funding Number(s)
CONTRACT_GRANT: NAS1-7154
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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