Multi-turbine engine aircraft developed by McDonnell Aircraft Corp, St.Louis, Mo, has empty weight of 2400 lb and takeoff gross weight of 6300 lb; useful load is 62% of gross weight, achieved by using pressure jet powered rotor; compressed air for pressure jets supplied by three AiResearch GTC-85-35 gas turbine compressors.
McDonnell's private venture model 120
Am Helicopter
American Helicopter ; 52 , n 10
1958
Aufsatz (Zeitschrift)
Englisch
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