首页> 美国政府科技报告 >HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM VOLUME ⅩⅢ PRELIMINARY MODEL SPECIFICATION FOR CONTINENTAL MODEL 357-1 ENGINE
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HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM VOLUME ⅩⅢ PRELIMINARY MODEL SPECIFICATION FOR CONTINENTAL MODEL 357-1 ENGINE

机译:重型提升涡轮增压器转子系统体积ⅩⅢ大陆模型357-1发动机的初步模型规范

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Volume XIII of a report entitled "Heavy-Lift Tip Turbojet Rotor System contains Continental Preliminary Model Specification No. 2253-A, which contains re¬quirement, capability, and engine performance data on the Continental Model 357-1 (1700-pound thrust) turbojet engine for helicopter rotor-tip mounting.

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