Hydrostatic Damper for the Space Shuttle Main Engine (SSME) High Prressure Oxidizer Turbopump (HPOTP)

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Report Number: WRDC-TR-89-3116 Volume I p. DBC-1
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
Pages: 28
Contract: Laboratory Research - No Contract
DoD Project: 486U
DoD Task: 11
Identifier: This paper is part of a conference proceedings. See ADA309668

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Provenance: Bombardier/Aero

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