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STS-1 Pogo analysisSome of the pogo related data from STS-1 are documented. The measurements and data reduction are described. In the data analysis reference is made to FRF and single engine test results. The measurements are classified under major project elements of the space shuttle main engine, the external tank, and the orbiter. The subsystems are structural dynamics and main propulsion. Data were recorded onboard the orbiter with a minimum response rate of 1.5 to 50 Hz. The wideband, 14 track recorder was used, and the data required demultiplexing before reduction. The flight phase of interest was from liftoff through main engine cutoff.
Document ID
19850011697
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Date Acquired
September 5, 2013
Publication Date
June 1, 1981
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TM-87433
NAS 1.15:87433
Report Number: NASA-TM-87433
Report Number: NAS 1.15:87433
Accession Number
85N20007
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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