V-22 Specifications

Powerplant
  • Two Allison T406-AD-400 engines
  • Max and Intermediate, shp (kW) - 6,150 (4,586)

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)

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)
 

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)

New weapon system being developed for deployment with the V-22 Osprey

The Expeditionary Fire Support System is designed to deploy with the V-22 and provide fire support for Marines on the ground. Check out the photos below.

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