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)
• 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)
• Takeoff, self-deploy mission, lbs (kg)
• 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)