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PROPULSION SYSTEM EVALUATION THROUGH FLIGHT SIMULATIONApplication of a differential correction method for the evaluation of rocket propulsion systems by flight simulation techniques
Document ID
19630019147
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Jackson, J. W.
Date Acquired
August 1, 2013
Publication Date
March 20, 1963
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 63078-63
Report Number: AIAA PAPER 63078-63
Accession Number
63A15206
Distribution Limits
Public
Copyright
Other
Keywords
FLIGHT SIMULATION
ROCKET ENGINE
PROPULSION SYSTEM PERFORMANCE

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