Analytical evaluation of secondary flow injection effects on rocket engine performance including cold flow and simulated hot flow data
Analytical methods for computing the effects of turbine exhaust and film-coolant injection on rocket engine performance.
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE ; 1969 ; COLORADO SPRINGS, COLO.
1969-06-01
Conference paper
No indication
English
Failure analysis of reusable rocket engine coolant passage
British Library Online Contents | 2013
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