Nonlinear analysis of the space shuttle superlightweight LO₂ tank
Subtitle: presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Material Conference : Long Beach, California, April 20-23, 1998
By: Michael P. Nemeth ... [et al.].
Contributors: Nemeth, Michael P.; United States. National Aeronautics and Space Administration.; AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (1998 Long Beach, Calif.)
Series: NASA/TM -- 1998-208126.; NASA/TM -- 1998-20812.; NASA technical memorandum -- 208126.; NASA technical memorandum -- 208127.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1998
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Space shuttles.; Thin walls.; Loads (Forces); Liquid oxygen.; External tanks.; Cryogenic fluid storage.; Cryogenic temperature.
Notes: Shipping list no.: 99-0032-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 2 microfiches.
Table of contents: title: Pt. I. Behavior under booster ascent loads; title: Pt. II. Behavior under 3g end-of-flight loads.