V-22 Osprey
Technical Specs
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 (6,147 )
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)
