Space Shuttle main engine (SSME) LOX turbopump pump-end bearing analysis : final report.

Bibliographic Details

Corporate Authors:	SRS Technologies. Systems Technology Division, George C. Marshall Space Flight Center. Materials and Processes Laboratory
Format:	Government Document eBook
Language:	English
Published:	Huntsville, Ala. : Marshall Space Flight Center, Ala. : SRS Technologies, Systems Technology Division ; Materials and Processes Laboratory, Engineering Physics Division, George C. Marshall Space Flight Center, [1986]
Series:	NASA contractor report ; 178746.
Subjects:	Computerized simulation. Liquid oxygen. Space Shuttle Main Engine. Turbine pumps.
Online Access:	https://purl.fdlp.gov/GPO/gpo24147