Διαφορά μεταξύ των αναθεωρήσεων του «Nord Noratlas»

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imported>GraemeLeggett
imported>GraemeLeggett
|area alt= 101.2 m²
|airfoil=
|empty weight main= 2882528,825 lb
|empty weight alt= 1307513,075 kg
<!--|loaded weight main= lb
|loaded weight alt= kg-->
|useful load main=1864718,647 lb
|useful load alt=84588,458 kg
|max takeoff weight main= 4850048,500 lb
|max takeoff weight alt= 2200022,000 kg
|more general=
 
|thrust original=
|thrust more=
|afterburning thrust main= lbf
|afterburning thrust alt= kN
|engine (prop)=[[SNECMA]]-manufactured [[Bristol Hercules]] 738/739
|type of prop=[[Bristol Hercules]]radial 738/739engine
|number of props=2
|power main= 20402,040 hp
|power alt= 15201,520 kW
|power original=
|power more=
|cruise speed main=199 mph
|cruise speed alt=320 km/h
|cruise speed more=at 15001,500 meters
<!--|never exceed speed main= mph
|never exceed speed alt= km/h
|stall speed main= mph
|stall speed alt= km/h
|stall speed more=-->
|range main=15501,550 mi
|range alt=25002,500 km
|range more=
|ceiling main=2330023,300 ft
|ceiling alt=71007,100 m
|climb rate main=10801,080 ft/min
|climb rate alt=5.5 m/s
<!--|loading main= lb/ft²
|loading alt= kg/m²
|thrust/weight=
|power/mass main= hp/lb
|power/mass alt= kW/kg-->
|more performance=
 
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