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Stability codes for a liquid rocket implemented for use on a PCThe high frequency code has been made an interactive code using FORTRAN 5.0. The option to plot n-tau curves was added using the graphics routines of FORTRAN 5.0 and GRAFMATIC. The user is now able to run with input values non-dimensional (as in the original code) or dimensional. Input data may be modified from the keyboard. The low and intermediate frequency codes have been run through a set of variations. This will help the user to understand how the stability of a configuration will change if any of the input data changes.
Document ID
19930003471
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Armstrong, Wilbur
(Alabama Univ. Huntsville, AL, United States)
Doane, George C., III
(Alabama Univ. Huntsville, AL, United States)
Dean, Garvin
(Alabama Univ. Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:184453
NASA-CR-184453
Report Number: NAS 1.26:184453
Report Number: NASA-CR-184453
Accession Number
93N12659
Funding Number(s)
CONTRACT_GRANT: NAS8-36955
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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