Aeroplane and Commercial Aviation News, 107. kötet1964 |
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20. oldal
... weight ) 75.3 lb / ft2 ( 369 kg / m2 ) Wing loading ( max . landing weight ) 60-8 lb / ft2 ( 297 kg / m2 ) Thrust loading ( max . take - off weight ) 3-4 lb / lb s.t. ( 3.4 kg / kg s.t. ) Design Criteria PAYLOAD THOUSAND LB. US CENTS ...
... weight ) 75.3 lb / ft2 ( 369 kg / m2 ) Wing loading ( max . landing weight ) 60-8 lb / ft2 ( 297 kg / m2 ) Thrust loading ( max . take - off weight ) 3-4 lb / lb s.t. ( 3.4 kg / kg s.t. ) Design Criteria PAYLOAD THOUSAND LB. US CENTS ...
23. oldal
... WEIGHT COMPARISON Structure Mach 3-0 Mach 2-2 Powerplant Systems 67 000 40 900 29 850 90 900 42.000 35 500 Total equipped weight inc . crew 140 000 Payload Fuel 25 200 159 800 172 650 25 200 192.500 Gross weight 325 000 Landing weight ...
... WEIGHT COMPARISON Structure Mach 3-0 Mach 2-2 Powerplant Systems 67 000 40 900 29 850 90 900 42.000 35 500 Total equipped weight inc . crew 140 000 Payload Fuel 25 200 159 800 172 650 25 200 192.500 Gross weight 325 000 Landing weight ...
27. oldal
... weight of 2 110 lb , a useful load of 1 490 lb and a gross weight of 3 600 lb. The empty weight of 2 110 lb compares with that of 1 690 lb for the standard Comanche 250 . Fuel is carried in four rubber fuel cells - two 25 Imp . gal ( 30 ...
... weight of 2 110 lb , a useful load of 1 490 lb and a gross weight of 3 600 lb. The empty weight of 2 110 lb compares with that of 1 690 lb for the standard Comanche 250 . Fuel is carried in four rubber fuel cells - two 25 Imp . gal ( 30 ...
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