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8. oldal
and ASTRONAUTICS AK de Havilland Trident Second - Generation Trimotor Turbojet has Maximum Potential Able to operate from 6,000 - ft . runways at max . all - up weight , the Trident with its very high percentage landing weight can cover ...
and ASTRONAUTICS AK de Havilland Trident Second - Generation Trimotor Turbojet has Maximum Potential Able to operate from 6,000 - ft . runways at max . all - up weight , the Trident with its very high percentage landing weight can cover ...
94. oldal
( without bleed ) for a weight of 285 lb. This corresponds to a thrust / weight ratio of 8.8 and takes into account the weight of a number of engine accessories and the fuel system . With an eight - stage axial compressor and two ...
( without bleed ) for a weight of 285 lb. This corresponds to a thrust / weight ratio of 8.8 and takes into account the weight of a number of engine accessories and the fuel system . With an eight - stage axial compressor and two ...
96. oldal
According to the experience gained in the project office at Shorts , a layout with separate engines is often slightly heavier -although there is not much to choose between the installed weights of the two systems .
According to the experience gained in the project office at Shorts , a layout with separate engines is often slightly heavier -although there is not much to choose between the installed weights of the two systems .
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