Effect of Flange Bolt Preload on Space Shuttle Main Engine High Pressure Oxidizer Turbopump Housing Analysis

Effect of Flange Bolt Preload on Space Shuttle Main Engine High Pressure Oxidizer Turbopump Housing Analysis

Author(s):

Min, J.B. ( George C. Marshall Space Flight Center )
Johnston, L.M.
Czekalski, B.

Publication title:

NASA Technical Reports

Pub. Year:

1991

Issue:

NASA-TM-103536

Pt.:

NAS 1.15:103536

Paper no.:

N91-24584

Page(from):

1

Page(to):

36

Pages:

36

Pub. info.:

National Aeronautics and Space Adminstration

Language:

English

Type:

Technical Paper

Details

TDL ID:

ZA00001427

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