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Space engine performance prediction.Nozzle stagnation pressure and combustion efficiency determination for spacecraft engines using thrust measurements
Document ID
19650041734
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Mckevitt, F. X.
Walsh, T. J.
Date Acquired
August 2, 2013
Publication Date
June 1, 1965
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 64-267
Report Number: AIAA PAPER 64-267
Accession Number
65A24438
Funding Number(s)
CONTRACT_GRANT: NAS7-136
Distribution Limits
Public
Copyright
Other
Keywords
PERFORMANCE PREDICTION
SPACECRAFT PROPULSION

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