Fluid flow analysis of the SSME high pressure fuel and oxidizer turbine coolant systems
By: by G.A. Teal.
Contributors: Huntsville Engineering Center.; United States. National Aeronautics and Space Administration.
Series: NASA-CR -- 183736.; LMSC-HEC TR -- F 268780.; NASA contractor report -- NASA CR-183736.
Publisher: Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center
Published: 1990
Place of publication: Huntsville, AL
Language: eng
Format: Microform
Subjects: Engines -- Cooling.; Space shuttles.
Notes: Distributed to depository libraries in microfiche.

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