CMV-22B Osprey  
Initial Operational Capability (IOC): 2021
Total Production: 44
Origin: United States of America
Corporations: Bell Helicopter and Boeing
Parent System: V-22 Osprey
Initial Operational Capability (IOC): 2007
Total Production: 459
Total Cost: USD$53 billion
Family Members: CV-22B Osprey, HV-22A Osprey and MV-22B Osprey
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Description: The V-22 Osprey is a multi-mission, tilt-rotor aircraft with vertical takeoff and landing (VTOL) capability. It performs VTOL missions as effective as a conventional helicopter while also having the long range cruise abilities of a twin-turboprop aircraft. The V-22 features a tilt-rotor mounted on each wing tip with its corresponding engine/transmission nacelle. It can operate as a helicopter for takeoff and landing operations and otherwise required. Once airborne, the nacelles rotate forward 90-degree for horizontal flight, converting the V-22 to a high-speed airplane. The V-22's wing rotates for compact storage aboard ships. The V-22 will carry cargo externally and internally and will be armed with two 12.7mm guns. For improved survivability the V-22 includes cross-coupled transmissions so either engine can power the rotors if one engine fails.

The US Navy CMV-22B tiltrotor aircraft is a derivative of the US Marine Corps MV-22B Osprey and has been designed as the replacement for the C-2 Greyhound introduced in the 1960s. The modified CMV-22B has 200 nautical miles extra range to perform carrier onboard delivery (COD) missions carrying personnel, supplies and weapons. The US Navy expects to procure 44 CMV-22Bs to replace 35 C-2 aircraft beginning in 2021.

CMV-22B Osprey Specifications

Crew: 2
Number of Engines: 2
Dimensions
Height: 6.63 meter (21.8 foot)
Length: 17.5 meter (57 foot)
Wingspan: 25.6 meter (84 foot)
Performance
Ceiling: 7,925 meter (26,001 foot)
Max Range: 2,300 nautical mile (2,647 mile)
Power
Max Power at TakeOff: 12,300 shp (9,176 kW)
Speed
Top Speed at High Altitude: 351 mph (305 KTAS)
Weight
Cargo: 9,072 kilogram
Empty Weight: 15,032 kilogram (33,139 pound)
Max Takeoff Weight: 27,443 kilogram (60,500 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Operators & Related Equipment


OperatorsItems

Grand Total 441
Propulsion Systems
AE 1107Cx2
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