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Title Space Shuttle main engine (SSME) LOX turbopump pump-end bearing analysis [electronic resource] : final report .

Imprint

Huntsville, Ala. : SRS Technologies, Systems Technology Division ; Marshall Space Flight Center, Ala. : Materials and Processes Laboratory, Engineering Physics Division, George C. Marshall Space Flight Center, [1986]

Connect to
Connect to https://permanent.fdlp.gov/gpo24147/19860013162-1986013162.pdf
Connect to https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19860013162.pdf

Copies

Location	Call No.	OPAC Message	Status
Axe Federal Documents Online	NAS 1.26:178746	---	Available

Description	1 online resource (v, 52 p.) : ill.
Series	[NASA contractor report] ; 178746
	NASA contractor report ; 178746.
Note	Title from title screen (viewed on June 28, 2012).
	"January 6, 1986."
Type Of Report	Final report.
Funding	Prepared for Materials and Processes Laboratory, George C. Marshall Space Flight Center contract number NAS8-36183 Modification No. 6 SRS/STD-TR86-007
Subject	Computerized simulation.
	Liquid oxygen.
	Space Shuttle main engine.
	Turbine pumps.
Added Author	SRS Technologies. Systems Technology Division.
	George C. Marshall Space Flight Center. Materials and Processes Laboratory.
Other Form:	Print version: Space Shuttle main engine (SSME) LOX turbopump pump-end bearing analysis. (OCoLC)796997308
	Microfiche: Space Shuttle main engine (SSME) LOX turbopump pump-end bearing analysis. (OCoLC)796996040
Gpo Item No.	0830-H-14 (online)
Sudoc No.	NAS 1.26:178746