| Official
Designation |
V-22A Osprey |
| Service Designations |
CV-22 (USAF), HV-22 (USN), MV-22 (USMC) |
| Primary
Role |
Tactical V/STOL transport |
| Secondary
Role |
Special operations |
| National
Origin |
USA |
| Original
Contractor |
Bell Helicopter Textron and The Boeing Company |
| Operator |
United States Air Force, Navy, Marine Corps |
Dimensions
(spread configuration) |
Length: 57 feet, 4 inches (17.47m);
Width: 84 feet, 7 inches (25.76m);
Height: 22 feet, 7 inches (6.86m) |
Dimensions
(folded configuration) |
Length: 62 feet, 7 inches (19.05m);
Width: 18 feet, 5 inches (5.61m);
Height: 18 feet (5.47m) |
| Wingspan |
45 feet, 10 inches (13.96m) |
| Height
at
Tail |
17 feet, 7 inches (5.34m) |
| Cargo
Hold |
Length: 24 feet, 4 inches (7.41m);
Width: 5 feet, 11 inches (1.80m);
Height: 6 feet (1.83m) |
| Armament |
Varies |
| Engines |
Two Allison T406-AD-400 engines |
| Horsepower |
6,150 shp (4,588kW) per engine |
| Cruise
Speed |
316 mph (509km/h) in airplane mode;
213 mph (343km/h) in helicopter mode |
| Max
Speed |
Unknown |
Range
(self deployment) |
2,100 nm (3,889km) |
| Service
Ceiling |
26,000 feet (7,925m) |
| Operating
Weight |
33,140 pounds (15,032kg) |
| Fuel
Capacity |
13,850 pounds (6,282kg) |
| Max
Payload |
Internal: 20,000 pounds (9,072kg);
External: 10,000 pounds (4,526kg) per hook;
Rescue Hoist: 600 pounds (272kg) |
| Number
of
Seats |
24 |
| Max
Takeoff
Weight |
Vertical: 52,870 pounds (23,981kg);
Short-running: 57,000 pounds (25,855kg);
Self deployment: 60,500 pounds (27,442kg) |
| Basic
Crew |
Three (pilot, co-pilot, crew chief) |
| Date
Deployed |
Unknown |
| Total
in
Service |
Unknown |
|
|
|
