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.
APA Citation
Stabe, R. G., Kline, J. F., Lewis Research Center., United States. National Aeronautics and Space Administration. (1968). Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine. Washington, D.C.: National Aeronautics and Space Administration .
MLA Citation
Stabe, Roy G, John F Kline, Lewis Research Center, and United States. National Aeronautics and Space Administration. Cold-air Performance Evaluation of Scale Model Oxidizer Pump-drive Turbine for the M-1 Hydrogen-oxygen Rocket Engine. Washington, D.C.: National Aeronautics and Space Administration , 1968.
Warning: These citations may not always be complete (especially for serials).