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V-22
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General Characteristics:
Wingspan: 50.92 ft Weight: 55,000 lbs (VTOL/STOL), 60,500 lbs (Self Deploy STO) Power: 2 x Allison T406-AD-400 6,150 shp Rotor: 38 Feet wide, Graphite/Fiberglass construction Speed: 275 knots Climb: 2,320 feet per minute max Crew: 2 Passenger Capacity: 24 Fully-Equipped troops or 12 litters Ceiling: 26,000 ft max, 11,300 ft (one engine) Range: 515 Nautical Miles Take-Off Weight: 60,500 lbs max Empty Weight: 33,140 lbs Cargo Hook: 15,000 lbs max Length: 57.33 ft Width: 83.33 ft (rotors turning) Sponson Fuel Cap.: 1,228 Gals Wing Fuel Cap.: 787 Gals Miscellaneous Other Features
The US armed services plan on using this aircraft in a myriad of different environments. To be specific: Marines Designation: MV-22 Purpose: Amphibious assault transport of troops, equipment, and supplies from assault ships and land bases. Navy Designation: HV-22 Purpose: Strike Rescue, delivery and retrieval of special warfare teams, and logistics transportation in support of the fleet. Air Force Designation: CV-22 Purpose: Long Range special operations missions, insertion and extraction of special forces teams and equipment at mission radii in excess of 500 nm. Army Designation: MV-22 Purpose: Aeromedical evacuation, special operations, long range combat logistics support, combat air assault and low intensity conflict support. For More Information (and thumbnail photographs!), check: Bell's V22 Photo Archive and be sure to say hi to Kevin Hale and the Visual Arts people - they're the ones kind enough to send me Bell Stock photography for your viewing pleasure! |
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© 2001 The RotorHead |
at 800 x 600 resolution http://www.rotorhead.org File: /military/v22.asp |
Last change: 4/9/2007 |