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Program user's manual for optimizing the design of a liquid or gaseous propellant rocket engine with the automated combustor design code AUTOCOMThis computer program manual describes in two parts the automated combustor design optimization code AUTOCOM. The program code is written in the FORTRAN 4 language. The input data setup and the program outputs are described, and a sample engine case is discussed. The program structure and programming techniques are also described, along with AUTOCOM program analysis.
Document ID
19740008379
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Reichel, R. H. (Aerophysics Research Corp. Bellevue, WA, United States)
Hague, D. S. (Aerophysics Research Corp. Bellevue, WA, United States)
Jones, R. T. (Aerophysics Research Corp. Bellevue, WA, United States)
Glatt, C. R. (Aerophysics Research Corp. Bellevue, WA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1973
Publication Information
Publisher: NASA
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-2293
Report Number: NASA-CR-2293
Accession Number
74N16492
Funding Number(s)
CONTRACT_GRANT: NAS3-13331
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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