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Post Flight Dynamic Analysis SimulationDigital six-degrees-of-freedom, open loop Saturn 5 first stage flight evaluation simulation program obtains post flight simulation of the launch vehicle using actual flight data as input. Results are compared with measured data. For preflight analysis, the program uses predicted flight data as input.
Document ID
19700000585
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Gregory, B. R.
(BOEING CO.)
Date Acquired
August 5, 2013
Publication Date
November 1, 1970
Subject Category
Mathematics And Information Sciences
Report/Patent Number
MFS-15067
Report Number: MFS-15067
Accession Number
70B10605
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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