Structural evaluation of a space main engine (SSME) high pressure fuel turbopump turbine blade
By: Ali Abdul-Aziz.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- 198428.; NASA contractor report -- NASA CR-198428.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1996
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Space shuttle main engine; Finite element method; Structural analysis; Thermal analysis; Turbine blades; Turbine pumps; Mechanical properties
Notes: Shipping list no.: 98-0830-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.