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Exploring in aerospace rocketry. 7 - Liquid propellant rocket systemsOperating characteristics and design aspects of injector, combustion chamber, and exhaust nozzle for bipropellant rockets
Document ID
19680008657
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Conrad, E. W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1968
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-52394
Report Number: NASA-TM-X-52394
Meeting Information
Meeting: LEWIS AEROSPACE EXPLORERS
Location: CLEVELAND
Start Date: January 1, 1966
End Date: December 31, 1967
Accession Number
68N18126
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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