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Integrated model development for liquid fueled rocket propulsion systemsAs detailed in the original statement of work, the objective of phase two of this research effort was to develop a general framework for rocket engine performance prediction that integrates physical principles, a rigorous mathematical formalism, component level test data, system level test data, and theory-observation reconciliation. Specific phase two development tasks are defined.
Document ID
19940022663
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Santi, L. Michael
(Christian Brothers Coll. Memphis, TN, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1993
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-195253
NAS 1.26:195253
Accession Number
94N27166
Funding Number(s)
CONTRACT_GRANT: NAG8-212
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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