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Propulsion System Integration and Test Program (Steady State)-Summary. Part I. Integration Technique and Test Activities.
Final technical rept. Jun 67-Feb 69,
NORTH AMERICAN ROCKWELL CORP LOS ANGELES CA LOS ANGELES DIV
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The report describes a propulsion systemairplane integration technique and summarizes the results of six test programs conducted during the study. The six tests were Thrust divertervectoring system flow tests Shared exit ejector nozzle static tests Nozzle interaction drag tests Inlet drag tests Low speed auxiliary inlet tests and YTF-33 turbofan engine tests. Author
APPROVED FOR PUBLIC RELEASE