Thermal performance of a liquid hydrogen tank multilayer insulation system at warm boundary temperatures of 630, 530 and 152⁰ R
By: Robert J. Stochl and Richard H. Knoll.
Contributors: Knoll, Richard H.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 104476.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1991
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Fuel tanks.; Heat transfer.; Leakage.; Liquid hydrogen.; Multilayer insulation.; Temperature effects.
Notes: Distributed to depository libraries in microfiche.

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