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A new approach for evaluating the performance and base environment characteristics of nonconventional rocket propulsion systems.Nonconventional rocket propulsion systems performance and base environment characteristics evaluated, using separate cold flow and combustion models
Document ID
19670041343
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hendershot, K. C.
Sergeant, R. J.
Wilson, H. B., Jr.
Date Acquired
August 3, 2013
Publication Date
February 1, 1967
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 67-256
Report Number: AIAA PAPER 67-256
Accession Number
67A20072
Funding Number(s)
CONTRACT_GRANT: NAS8-20027
CONTRACT_GRANT: NAS8-823
Distribution Limits
Public
Copyright
Other
Keywords
PROPULSION SYSTEM PERFORMANCE
ENGINE TESTING
NOZZLE FLOW

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