Martin B-26 G "Marauder"

[David]

Martin B-26 G "Marauder"

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Country of Service :	United States
Role :	Medium Bomber
First Flight :
Production Date :
In-Service Date :	November 1942
Manufacturer :	Glenn L. Martin Company
Number Produced :	893
Crew :	7
Length :	17.09 meters
Height :	6.2 meters
Empty Weight :	11476 kilograms
Operational Weight :	17328 kilograms
Maximum Weight :	kilograms
Wing Span :	21.64 meters
Wing Aspect Ratio :	7.66
Wing Area :	61.13 square meters
Wing Load :	283.46 kg per square meter
Engine Number :	2
Engine Name :	Pratt & Whitney R-2800-3 Double Wasp
Coolant :	Air
Cylinders:	R-18
Capacity:	45.9 Liters
Power :	2000 hp @ 2800 rpm
Power / Weight Ratio :	230.84 hp per tonne
Max Speed :	455 kph @ 1524 meters
Cruising Speed :	348 kph @ 1524 meters
Climb :	305
Service Ceiling :	6035 meters
Range :	1770 kilometers
Fuel Capacity :	3566 liters
Machinegun Armament :	5x 12.7mm Browning (Forward Firing) 2x 12.7mm Browning (Ventral Turret) 2x 12.7mm Browning (Dorsal Turret) 2x 12.7mm Browning (Waist)
Cannon Armament :	None
Payload :	1814 kg (Internal)
Gunsight :	None
Avionics :	SCR-595A IFF Transponder T-1 Bombsight
Pilot Armor :	Yes
Self-Sealing Fuel Tanks :	Yes
Armored Windscreen :	Yes