Space shuttle main engine structural analysis and data reduction/evaluation. final report / Volume 2. High pressure oxidizer turbo-pump turbine end bearing analysis :

Bibliographic Details
Main Author:	Sisk, Gregory A. (Author)
Format:	Government Document eBook
Language:	English
Published:	Huntsville, AL : Lockheed Missiles & Space Company, Huntsville Engineering Center, 1989.
Series:	NASA contractor report ; NASA CR-183664.
Subjects:	Data reduction. Finite element method. Space shuttles > Propulsion systems. Structural analysis (Engineering) Turbine pumps. Synthetic training devices. Spacecraft propulsion. Computerized simulation. Space Shuttle Main Engine. Structural analysis.
Online Access:	https://purl.fdlp.gov/GPO/gpo176321

Description
Item Description:	"April 1989." "LMSC-HEC TR F268584-II." GPO Cataloging Record Distribution Program (CRDP).
Physical Description:	1 online resource (approximately 85 pages) : illustrations.
Bibliography:	Includes bibliographical reference (page 6).