HV-22A Osprey  
Initial Operational Capability (IOC): 2009
Total Production: 48
Unitary Cost: USD$116 million
Origin: United States of America
Corporations: Boeing and Textron
Parent System: V-22 Osprey
Initial Operational Capability (IOC): 2007
Total Production: 459
Total Cost: USD$53 billion
Family Members: CMV-22B Osprey, CV-22B 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 HV-22A will provide long range combat search and rescue, delivery and retrieval of special warfare teams along with fleet logistic support transport. The US Navy plans call for procurement of up to 48/49 HV-22s. In early 2015 the US Navy made public its intention to buy 44 V-22 aircraft of a new model.

HV-22A Osprey Specifications

Crew: 2
Number of Engines: 2
Troops: 24
Dimensions
Height: 6.63 meter (21.8 foot)
Length: 17.5 meter (57 foot)
Main Gun Caliber: 12.7 millimeter
Wingspan: 25.6 meter (84 foot)
Performance
Ceiling: 7,925 meter (26,001 foot)
Max Range: 3,889 kilometer (2,100 nautical mile)
Min Range: 954 kilometer (593 mile)
Power
Max Power at TakeOff: 12,300 shp (9,176 kW)
Speed
Top Speed at High Altitude: 142 mps (276 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)

HV-22A Osprey News

There are 6 news between
31 Mar 2004 and 27 Jan 2009
Tuesday, January 27, 2009Bell Boeing Team Awarded Joint Performance Based Logistics Contract for V-22 Osprey Support
Tuesday, January 23, 2007Boeing Awarded Contract for Next Generation V-22 Hydraulic Automated Test System
Tuesday, March 21, 2006First CV-22 Block 10 Handed Over to US Air Force
Friday, September 23, 2005Boeing Awarded Contracts for Joint Heavy Lift Program
Monday, September 19, 2005US Air Force Takes Delivery of First Production CV-22 Tilt-Rotor Aircraft
Wednesday, March 31, 2004V-22 Testing Air-to-Air Refueling Capability

Operators & Related Equipment


OperatorsItems

Grand Total 481
Propulsion Systems
AE 1107Cx2
Protection Systems
AN/ALQ-211 SIRFCx1
Sensor Systems
AN/AAQ-16x1
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