Technical Specs
Powerplant
- Two Rolls Royce AE1107C turboshaft 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) -- 38.08 (11.6)
- Blade folding - automatic, powered
Transmissions
- Takeoff VTOL, Normal Power 4570 rhp
- Takeoff VTOL, Interim Power 5183 rhp
Performance @ 47,000 lbs
- Max speed, SL, kts (km/h) -- 250 (463)
- Max rate of climb, SL, fpm (m/m)
3,200 (975) - Service ceiling, ft (m) -- 25,000 (7,620)
- Service ceiling, one engine inop, ft (m) -- 10,300 (3,139)
- HOGE, ft (m) -- 5,400 (1,646)
Range
- Unrefueled mission radius with 24 troops, nm (km) -- 390 (722)
- Self-deployment, nm (km) -- > 2,100 (3,892) with refueling
Crew
- Cockpit -- crew seats -- 2/3
- Cabin -- crew chief and troop seats/litters -- 1 + 24/12
Dimensions -- Internal
- Length, max, ft (m) -- 20.8 (6.34)
- Width, max, ft (m) -- 5.7 (1.74)
- Height, max, ft (m) -- 5.5 (1.67)
Weights
- Takeoff, vertical, max, lbs -- 52,600 (23,859)
- Takeoff, short running, max, lbs (kg)
57,000 (25,855) - 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) -- 84.6 (25.78)
- Length, stowed, ft (m) -- 63.1 (19.23)
- Width, stowed, ft (m) -- 18.5 (5.64)
- Height, nacelles fully vertical, ft (m) -- 22.1 (6.74)
- Height, vertical stabilizer, ft (m) -- 17.65 (5.38)
Fuel Capacity
- MV-22 gals (liters) -- 1,721 (6,513)
- CV-22 gals (liters) -- 2,037 (7,710)
- Aux, self-deployment, gals (liters) -- up to 3 tanks, each 430 (1,628)