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Orbital Maneuvering Engine Feed System Coupled Stability Investigation, Computer User's ManualAn operating manual for the feed system coupled stability model was given, in partial fulfillment of a program designed to develop, verify, and document a digital computer model that can be used to analyze and predict engine/feed system coupled instabilities in pressure-fed storable propellant propulsion systems over a frequency range of 10 to 1,000 Hz. The first section describes the analytical approach to modelling the feed system hydrodynamics, combustion dynamics, chamber dynamics, and overall engineering model structure, and presents the governing equations in each of the technical areas. This is followed by the program user's guide, which is a complete description of the structure and operation of the computerized model. Last, appendices provide an alphabetized FORTRAN symbol table, detailed program logic diagrams, computer code listings, and sample case input and output data listings.
Document ID
19760024193
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Schuman, M. D.
(Rockwell International Corp. Canoga Park, CA, United States)
Fertig, K. W.
(Rockwell International Corp. Canoga Park, CA, United States)
Hunting, J. K.
(Rockwell International Corp. Canoga Park, CA, United States)
Kahn, D. R.
(Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1975
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
R-9808
NASA-CR-150944
Report Number: R-9808
Report Number: NASA-CR-150944
Accession Number
76N31281
Funding Number(s)
CONTRACT_GRANT: NAS9-14315
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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