High pressure oxidizer turbopump (HPTOP) inducer dynamic design environment [microform] / D.A. Herda, R.S. Gross.

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Bibliographic Details
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Main Author:	Herda, D. A.
Corporate Author:	George C. Marshall Space Flight Center
Other Authors:	Gross, R. S.
Format:	Government Document Book
Language:	English
Published:	MSFC, Ala. : [Springfield, Va.] : National Aeronautics and Space Administration, Marshall Space Flight Center ; [National Technical Information Service, distributor], [1995]
Series:	NASA technical paper ; 3589.
Subjects:	Engine design. High pressure. Impellers. Oxidizers. Space shuttle main engine. Strain measurement. Turbine pumps.

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Call Number:	NAS 1.60:3589
NAS 1.60:3589	Available