Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine. :

Stabe, Roy G.

Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine. : - - Washington, D.C. NASA 1966 - 27 - NASA TP - 1624 : 1980 .







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