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V-22 Specifications
Powerplant
Two Allison T406-AD-400 engines
Max and Intermediate, shp (kW) - 6,150 (4,586)
Rotor System
Blades per hub - 3
Construction - graphite/fiberglass
Tip speed, fps (mps) - 661.90 (201.75)
Diameter, ft (m) - 38.00 (11.58)
Blade area, ft2 (m2) - 261.52 (24.30)
Disc area, ft2, (m2) - 2,268.00 (210.70)
Blade folding - automatic, powered
Transmissions
Takeoff [USMC], shp (kW) - 4,570 (3,408)
Takeoff [USN], shp (kW) - 4,970 (3,706)
Takeoff [USAF], shp (kW) - 4,970 (3,706)
1 engine inoperative, shp (kW) - 5,920 (4,415)
Performance
Max speed, SL, kts (km/h) - 275 (510)
Vert rate of climb, SL, fpm (m/m) 1,090 (332)
Max rate of climb, SL, fpm (m/m) 2,320 (707)
Service ceiling, ft (m) - 26,000 (7,925)
Service ceiling, one engine inop, ft (m) 11,300 (3,444)
HOGE, ft (m) - 14,200 (4,328) Range
Amphib assault, nm (km) - 515 (954)
Max, self-deployment, nm (km) 2,100 (3,892) Crew
Cockpit - crew seats - 2
Cabin - troop seats/litters - 24/12
Dimensions - Internal
Length, max, ft (m) - 24.17 (7.37)
Width, max, ft (m) - 5.92 (1.80)
Height, max, ft (m) - 6.00 (1.83) Weights
Empty, lbs (kg) - 33,140 (15,032)
Takeoff, vertical, max, lbs - 47,500 (21,546)
Takeoff, short running, max, lbs (kg) 55,000 (24,948)
Takeoff, self-deploy mission, lbs (kg) 60,500 (27,443)
Cargo hook, single, lbs (kg) 10,000 (4,536)
Cargo hook, dual, lbs (kg) - 15,000 (9,221)
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Range
Amphib assault, nm (km) - 515 (954)
Max, self-deployment, nm (km) 2,100 (3,892)
Crew
Cockpit - crew seats - 2
Cabin - troop seats/litters - 24/12
Dimensions - External
Length, fuselage, ft (m) - 57.33 (17.48)
Width, rotors turning, ft (m) - 83.33 (25.55)
Length, stowed, ft (m) - 62.58 (19.08)
Width, stowed, ft (m) - 18.42 (5.61)
Width, horizontal stabilizer, ft (m) - 18.42 (5.61)
Height, nacelles fully vertical, ft (m) - 21.76 (6.63)
Height, vertical stabilizer, ft (m) - 17.65 (5.38)
Fuel Capacity
Sponsons, gals (liters) - 1,228 (4,649)
Wings, gals (liters) - 787 (2,979)
Aux, self-deployment, gals (liters) - 2,436 (9,221)
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