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User's manual for the ALS base heating prediction code, volume 2The Advanced Launch System (ALS) Base Heating Prediction Code is based on a generalization of first principles in the prediction of plume induced base convective heating and plume radiation. It should be considered to be an approximate method for evaluating trends as a function of configuration variables because the processes being modeled are too complex to allow an accurate generalization. The convective methodology is based upon generalizing trends from four nozzle configurations, so an extension to use the code with strap-on boosters, multiple nozzle sizes, and variations in the propellants and chamber pressure histories cannot be precisely treated. The plume radiation is more amenable to precise computer prediction, but simplified assumptions are required to model the various aspects of the candidate configurations. Perhaps the most difficult area to characterize is the variation of radiation with altitude. The theory in the radiation predictions is described in more detail. This report is intended to familiarize a user with the interface operation and options, to summarize the limitations and restrictions of the code, and to provide information to assist in installing the code.
Document ID
19930013773
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Reardon, John E.
(Remtech, Inc. Huntsville, AL, United States)
Fulton, Michael S.
(Remtech, Inc. Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:192457
RTR-218-01-VOL-2
NASA-CR-192457
Report Number: NAS 1.26:192457
Report Number: RTR-218-01-VOL-2
Report Number: NASA-CR-192457
Accession Number
93N22962
Funding Number(s)
CONTRACT_GRANT: NAS8-38141
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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