High Gallery
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U. S. Military Aircraft
Bell/Boeing V-22 OSPREY Photo by Coll B Thouanel |
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For some 40 years Bell has explored the Convertiplane concept in which two or more engines and their associated propeller/rotor assemblies can be swiveled between the vertical and the horizontal to provide direct lift or level thrust. Proved as early as 1958 by the XV-3 research machine, the concept was shown to be practical by the XV-15 of the late 1970's. Bell then teamed with Boeing for the JVX (Joint Services Advanced Vertical Lift Aircraft), a multi role convertiplane based on XV-15 Technology. The first of six V-22 prototypes flew in helicopter mode during March 1989, and the first full conversion to plane mode was achieved in September. This type has very considerable capabilities, but the whole program has been troubled by changing political and economic commitments. As of early 2000 three test aircraft had crashed: no one was killed in the 1991 crash, an accident in 1992 killed seven men, and the third in April 2000 killed 19 Marines. |
TECHNICAL DATA
| Description | Specifications |
| Manufacturer: Boeing Defense and Space Group, Philadelphia, PA, Bell Helicopter Textron, Ft Worth, TX, Allison Engine Company, Indianapolis, IN. | Length: 57 ft. 4 in. Spread |
| First Flight: March 1989 | Height: 22' 1" - Spread |
| Model: V-22 | Empty Weight: 30,850 lb. |
| Crew: Two | Max. Weight: 60,500 lb. |
| Nickname: Osprey | Pay Load: 24 troops or 15,000 lb. |
| Basic Role: Assault & logistic transport | |
| Other Versions: CV-22A: US Air Force special operation aircraft, HV-22A: Navy combat rescue Aircraft, MV-22A: US Marines Corps assault transport and US Army supply and case vac aircraft, SV-22A: proposed US Navy anti submarine aircraft. |
Dimensions |
| Principal User: United States | Propeller Rotor Diameter Each: 38 ft. 0 in. |
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Performance |
Propeller Rotor Horizontal : 20 ft. 2 in. |
| Range: 460 miles. | Propeller Rotor Disk Area: 2,268.23 sq. ft. |
| Max. Speed: 345 mph. |
Propulsion |
| Ceiling: 25,000 ft. | Power Plant: Allison T406-AD-400 turbo shaft. |
| Climb rate: 2,320 per min. | Horsepower: 6,160-shp (3,493 kW) |
| No. Of Engines: Two |