Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine.
IV,
Performance of first stage with modified inlet feedpipe-manifold assembly /
Roy G. Stabe, John F. Kline.

Description

Main Author: Stabe, Roy G.
Related Names: Kline, John F.
Lewis Research Center.
United States. National Aeronautics and Space Administration.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration ; 1968.
Subjects: Turbine pumps > Turbine pumps / Testing.
Rocket engines > Rocket engines / Models.
Note: Cover title.
"February 1968."
Physical Description: 21 p. : ill. ; 26 cm.
Locate a Print Version: Find in a library

Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign