High pressure oxidizer turbopump (HPTOP) inducer dynamic design environment
By: D.A. Herda, R.S. Gross.
Contributors: Gross, R. S.; George C. Marshall Space Flight Center.
Series: NASA technical paper -- 3589.
Publisher: National Aeronautics and Space Administration, Marshall Space Flight Center; National Technical Information Service, distributor
Published: 1995
Place of publication: MSFC, Ala; [Springfield, Va
Language: eng
Format: Microform
Subjects: Engine design.; High pressure.; Impellers.; Oxidizers.; Space shuttle main engine.; Strain measurement.; Turbine pumps.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0556-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1996] 1 microfiche.