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Hydrostatic Damper for the Space Shuttle Main Engine (SSME) High Prressure Oxidizer Turbopump (HPOTP)
Author(s): Goggin, David G., Beatty, Robert F., Scharrer, Joseph K.Corporate Author(s): Rockwell International
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1989-11
Report number: WRDC-TR-89-3116 Volume I p. DBC-1
full text available
Considerations of Synthesized System Damping in Dynamic Analysis of Space Structures
Author(s): Tsai, Wan T.Corporate Author(s): Rockwell International
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1989-11
Report number: WRDC-TR-89-3116 Volume I p. DBE-1
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