Orbital transfer vehicle oxygen turbopump technology. final report / Volume I, Design, fabrication, and hydrostatic bearing testing :

Bibliographic Details

Corporate Authors:	United States. National Aeronautics and Space Administration, Lewis Research Center
Other Authors:	Buckmann, P. S.
Format:	Government Document Book
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, [1990]
Series:	NASA contractor report ; NASA CR-185175.
Subjects:	Engine tests. High pressure oxygen. Hydrogen. Liquid oxygen. Orbit transfer vehicles. Oxygen. Rocket engine design. Turbine pumps.
Online Access:	https://purl.fdlp.gov/GPO/LPS60999