Final report on shuttle Centaur engine cool down evaluation and effects of expanded inlet on start transient
By: prepared by United Technologies Corporation, Pratt & Whitney, Government Products Division.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-183198.
Publisher: United Technologies, Pratt & Whitney; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1987
Place of publication: West Palm Beach, Fla; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Space shuttles -- Propulsion systems.
Other titles: Shuttle Centaur engine cool down evaluation and effects of expanded inlet on start transient.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 2 microfiches.