The structural dynamics analysis of the main injector LOX inlet tee and its redesign
By: [E. Romano].
Contributors: Rockwell International. Rocketdyne Division.; United States. National Aeronautics and Space Administration.
Series: NASA CR -- 186764.; NASA contractor report -- NASA CR-186764.
Publisher: Rockwell International, Rocketdyne Division?; National Aeronautics and Space Administration?
Published: 1989
Place of publication: [Canoga Park, Calif; Washington, D.C
Language: eng
Format: Microform
Subjects: Design analysis.; Dynamic response.; Dynamic structural analysis.; Injectors.; Intake systems.; Liquid oxygen.; Space shuttle main engine.; T shape.; Vanes.
Notes: Also available via Internet from the NASA Technical Report Server web site. Address as of 5/15/06: http://nrs.nasa.gov/archive/nasa/casi/ntrs.nasa.gov/19900017042%5F1990017042.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 1 microfiche.