Specifications |
Primary function | Amphibious assault transport of troops, equipment and supplies from assault ships and land bases
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Prime Contractor(s) | Boeing Defense and Space Group, Philadelphia, PA
Bell Helicopter Textron, Ft Worth, TX
Allison Engine Company, Indianapolis, IN
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Description | The V-22 Osprey is a multi-engine, dual-piloted, self-deployable, medium lift, vertical takeoff and landing (VTOL) tiltrotor aircraft designed for combat, combat support, combat service support, and Special Operations missions worldwide. It will replace the Corps' aged fleet of CH-46E and CH-53D medium lift helicopters
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Variants |
MV-22B Osprey - Standard naval production variant with ramp gun
MV-22C Osprey - Upgrade program with nose gun pod, avionics upgrade, and countermeasures upgrade for MV-22B
CV-22 is utilized by the Air Force for their Special Operations missions maintaining maximum commonality with the MV-22. Aircraft avionics peculiar to the Air Force unique mission requirements constitute aircraft differences.
CV-22B Osprey - Standard air force production variant with ramp gun
CV-22C Osprey - Upgrade program with nose gun pod, avionics upgrade, and countermeasures upgrade for CV-22B
HV-22 is used by the Navy the for Combat Search and Rescue and fleet logistics support.
UV-22 Army Variant - cancelled
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Length |
57' 4" - Spread
63' 0" - Folded
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Width |
84' 7" - Spread
18' 5" - Folded
38 feet 1 inch - Individual Tilt-rotor Diameter
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Height |
22' 1" - Spread
18' 1" - Folded
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Weights |
33,140 lb (15,032) Empty weight
52,600 lbs (23,860 kg) Takeoff, Vertical Takeoff/Landing (VTOL)
57,000 lbs (24,948 kg) Takeoff, Short Takeoff/Landing (STOL)
60,500 lbs (27,443 kg) Takeoff, Self Deploy STO (Maximum Take-Off)
10,000 lbs (4,536 kg) Cargo hook, single
15,000 lbs (6,804 kg) Cargo hook, dual
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Max fuel capacity | 2,037 gal/13,850 lbs
1,228 gals (4,649 liters) Sponsons
787 gals (2,979 liters) Wing
2,436 gals (9,221 liters) Aux, self-deployment
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Propulsion | Two AE1107C Rolls-Royce Allison @ 6,150 shp (4,586 kW)
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Transmissions |
Takeoff {USMC}, 4,570 shp (3,408 kW)
Takeoff {USN}, 4,970 shp (3,706 kW)
Takeoff {USAF}, 4,970 shp (3,706 kW)
1 engine inoperative, 5,920 shp (4,415 kW)
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Range |
200nm Pre-Assault Raid with 18 troops
200nm Land Assault with 24 troops
50 nm (x2) Amphibious Assault
500 nm Long Range SOF Missions (USAF/CV-22)
2,100 nm Self Deploy (with one refueling)
50 nm External Lift Operations with 10,000 lb load
SD-572 Mission | Threshold | MV-22 Block A |
Self - Deployment (3 x 430 gal) | 2,100 NM | 2,384 NM |
Pre - Assault Raid | 200 NM | 268.6 NM |
Amphib Assault - Troops | 50 NM | 82.2 NM |
Amphib Assault - External Cargo | 50 NM | 130.1 NM |
Land Assault - Troops | 200 NM | 245.9 NM |
Land Assault - Ext Cargo | 50 NM | 63.3 NM |
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Airspeed |
240 kts Cruise speed (MV-22)
230 kts Cruise speed (CV-22)
275 KTAS Cruise speed (3000'/91.5 deg F)
305 KTAS Max speed (15,000' /45 deg F)
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Rate of Climb |
1,090 fpm (332 m/m) Vertical rate of climb, SL
2,320 fpm (707 m/m) Max rate of climb, SL
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Ceiling |
25,000 ft (7,925 m) Service Ceiling
11,300 ft (3,444 m) Service Ceiling, OEI
14,200 ft (4,328 m) HOGE
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Cabin provisions | 24 troops/12 litters
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Rescue hoist capacity | 600 lbs
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Cargo floor limit | 300 PSF
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Milestones | First Flight - March 19, 1989
First Sea Trials - USS Wasp (LHD-1), December, 1990, Aircraft # 3 & 4
First EMD Flight - February 5, 1997
2nd Sea Trials - USS Saipan (LHA-2), January, 1999, Aircraft #10
First LRIP Delivery - May 25, 1999
OPEVAL - Scheduled October, 1999 to May, 2000
Full Rate Production - First Quarter, 2001
IOC - USMC - 2001;
IOC - US SOCOM - 2004
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Unit Cost | $40.1M (Total Program Recurring Flyaway, Constant Year, FY94$)
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Number Procured | 12 MV-22(authorized through FY98)
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Planned Inventory |
360 MV-22B (USMC)
50 CV-22A (USAF)
48 HV-22B (USN)
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Deployed to | MV-22s will be deployed to all Marine Corps medium lift active duty and reserve tactical squadrons, the medium lift training squadron (FRS), and the executive support squadron (HMX)
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