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SSME alternate turbopump (pump section) axial load analysisA flow balancing computer program constructed to calculate the axial loads on the Space Shuttle Main Engine (SSME) alternate turbopumps (ATs) pump sections are described. The loads are used in turn to determine load balancing piston design requirements. The application of the program to the inlet section, inducer/impeller/stage, bearings, seals, labyrinth, damper, piston, face and corner, and stationary/rotating surfaces is indicated. Design analysis results are reported which show that the balancing piston's designs are adequate and that performance and life will not be degraded by the turbopump's axial load characteristics.
Document ID
19890059586
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Crease, G. A.
(Pratt and Whitney Aircraft Group West Palm Beach, FL, United States)
Rosello, A., Jr.
(Pratt and Whitney Aircraft Group West Palm Beach, FL, United States)
Fetfatsidis, A. K.
(United Technologies Corp. Pratt and Whitney Group, West Palm Beach, FL, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1989
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 89-2607
Report Number: AIAA PAPER 89-2607
Accession Number
89A46957
Funding Number(s)
CONTRACT_GRANT: NAS8-36801
Distribution Limits
Public
Copyright
Other

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