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Aviation History
1951
1951 - 1213.PDF
Flight, 2<)June 1951 Y The pump will deliver petrol at 750 g.p.h. (maximum). Its stroke is varied by a hydraulic servo which is responsive to any required signal, thus giving complete control with rapid response in output. The barometric control maintains correct pump delivery pressure in accordance with variation in altitude and forward speed. FUEL AND COMBUSTION SYSTEMS FOR GAS TURBINE ENGINES
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