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High altitude chemically reacting gas particle mixtures. Volume 3: Computer code user's and applications manualA users manual for the RAMP2 computer code is provided. The RAMP2 code can be used to model the dominant phenomena which affect the prediction of liquid and solid rocket nozzle and orbital plume flow fields. The general structure and operation of RAMP2 are discussed. A user input/output guide for the modified TRAN72 computer code and the RAMP2F code is given. The application and use of the BLIMPJ module are considered. Sample problems involving the space shuttle main engine and motor are included.
Document ID
19850007494
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Smith, S. D.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1984
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:171828
NASA-CR-171828
LMSC-HREC-TR-D867400-3-VOL-3
Report Number: NAS 1.26:171828
Report Number: NASA-CR-171828
Report Number: LMSC-HREC-TR-D867400-3-VOL-3
Accession Number
85N15803
Funding Number(s)
CONTRACT_GRANT: NAS9-16256
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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