Effect of flange bolt preload on space shuttle main engine high pressure oxidizer turbopump housing analysis
By: by J.B. Min, L.M. Johnston, and B. Czekalski.
Contributors: Johnston, L. M.; Czekalski, B.; George C. Marshall Space Flight Center.
Series: NASA technical memorandum -- 103536.
Publisher: National Aeronautics and Space Administration, George C. Marshall Space Flight Center; For sale by the National Technical Information Service
Published: 1991
Place of publication: [Huntsville, Ala.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Bending fatigue.; Bolts.; Flanges.; Housings.; Load distribution (Forces); Prestressing.; Stress analysis.; Stress distribution.; Structural design.
Notes: Also available via Internet from the NASA Technical Report Server web site. Address as of 4/27/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910015270%5F1991015270.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991]. 1 microfiche.