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V-22 Osprey Bell/
Boeing
V-22 Osprey
VTOL Transport

DESCRIPTION:
The idea of uniting the vertical takeoff and landing capabilities of a helicopter with the high-speed cruise flight of an airplane has long intrigued aircraft designers. While many manufacturers have attempted to develop tiltrotors or "convertiplanes" with rotors at the wing tips able to pivot between "helicopter mode" and "airplane mode," the most successful company in this arena has been Bell.
Bell first explored the tiltrotor concept in the 1950s, but the idea did not attract military attention until the flight of the XV-15 research aircraft of the 1970s. This design, the first in which the entire rotor nacelle was pivoted, proved so successful that the Navy offered Bell and Boeing a contract to develop the concept into a transport aircraft for the Marine Corps.
The resulting V-22 has a conventional cabin for two flight crew and up to 24 fully armed troops or cargo pallets. The two engine nacelles are located at each end of a slightly forward swept wing and are able to pivot through 97.5°. For greater safety, the engines are connected through a complex series of gearboxes so that one engine can power both nacelles in case the other engine fails. The V-22 also folds into a compact size for ship storage by folding the propeller blades inward and rotating the entire wing parallel to the fuselage.
Due to its complexity and revolutionary design, the V-22 program has been plagued by technical difficulties, high cost, controversy, and the threat of cancellation. These issues were brought to a head in 2000 after two fatal accidents and revelations that Marine Corps officers had falsified maintenance records to improve the aircraft's readiness figures. These difficulties forced a two-year delay in the flight test program while the plane was grounded for modifications.
After a nearly 20 year development period, however, the aircraft finally began entering service with the Marine Corps in 2007. Current plans call for the Marines to purchase 360 units of the MV-22. The Navy is to introduce 48 aircraft starting in 2008 while the Air Force will buy 50 CV-22 models with service entry slated for 2009.
Last modified 26 October 2007

HISTORY:

First Flight 19 March 1989

Service Entry

June 2007

CREW: three: pilot, co-pilot, loadmaster

PASSENGERS: 24 troops

ESTIMATED COST:

$69.9 million [2006$]

AIRFOIL SECTIONS:

Wing Root Bell A821201 (23%)

Wing Tip Bell A821201 (23%)

Rotor Blade Root XN28/XN18/XN12

Rotor Blade Tip

XN09

DIMENSIONS:

Length 57.33 ft (17.47 m)

Wingspan 50.92 ft (15.52 m) including nacelles
84.50 ft (25.77 m) with rotors turning

Height 21.75 ft (6.63 m) with nacelles vertical

Rotor Diameter 38.00 ft (11.58 m) for each 3-bladed rotor

Wing Area 382 ft² (35.49 m²)

Rotor Disk Area 2,268 ft² (210.72 m²) total

Canard Area

not applicable

WEIGHTS:

Empty 33,140 lb (15,060 kg)

Normal Takeoff 47,500 lb (21,545 kg) [vertical TO]

Max Takeoff 52,870 lb (24,030 kg) [vertical TO]
57,000 lb (25,910 kg) [short TO, 20 deg tilt]
60,500 lb (27,500 kg) [short TO ferry]

Fuel Capacity internal: 13,850 lb (6,295 kg)
external: unknown

Max Payload

20,000 lb (9,090 kg) internally
15,000 lb (6,820 kg) externally
600 lb (272 kg) capacity rescue winch

PROPULSION:

Powerplant two Rolls-Royce/Allison AE1107C turboshafts

Thrust 12,300 shp (9,172 kW)

PERFORMANCE:

Max Level Speed at altitude: 390 mph (630 km/h) [airplane mode]
at sea level: 115 mph (185 km/h) [helicopter mode]

Initial Climb Rate 2,320 ft (705 m) / min

Service Ceiling 25,000 ft (7,630 m)

Hover Ceiling
(out of ground effect) 7,000 ft (2,135 m) [HV-22]
5,000 ft (1,525 m) [CV-22]

Range typical: 505 nm (935 km)
ferry: 2,100 nm (3,890 km)

g-Limits unknown

ARMAMENT:

Gun provision for two .50 caliber cabin guns

Stations two external hardpoints

Air-to-Air Missile none

Air-to-Surface Missile none

Bomb none

Other none

KNOWN VARIANTS:

MV-22 Baseline assault transport for the US Marines, also equipped for medical evacutaion (up to 12 litters), search-and-rescue, supply transport, and special operations; 408 to be built

HV-22 Search-and-rescue model for the US Navy, also equipped for special operations duties and fleet logistics; 48 originally planned but this model was cancelled as the Navy will purchase the standard MV-22 variant instead

CV-22 Special operations model for the US Air Force, able to covertly insert and extract up to 18 troops while flying 500 nm (925 km) at 500 ft (150 m) or lower altitude; 50 to be built

PRV-22 Combat search-and-rescue model proposed to the US Air Force as a replacement for the HH-60G Pavehawk; not developed

KNOWN COMBAT RECORD: Iraq - Operation Iraqi Freedom (USMC, 2007)

KNOWN OPERATORS: United States (US Air Force)
United States (US Marine Corps)
United States (US Navy)

3-VIEW SCHEMATIC:

V-22 Osprey

SOURCES:

Donald, David, ed. The Complete Encyclopedia of World Aircraft. NY: Barnes & Noble, 1997, p. 118, Bell/Boeing V-22 Osprey.

FAS V-22 site

Gunston, Bill and Spick, Mike. Modern Fighting Helicopters. London: Salamander Books, 1998, p. 96-97, Bell/Boeing V-22 Osprey.

_____. MV-22 Crash, Marine Corps Gazette, vol. 84, no. 5, May 2000, p. 10.

Osprey On-Line

US Navy V-22 Fact Sheet

Aircraft | Design | Ask Us | Shop | Search

DESCRIPTION: The idea of uniting the vertical takeoff and landing capabilities of a helicopter with the high-speed cruise flight of an airplane has long intrigued aircraft designers. While many manufacturers have attempted to develop tiltrotors or "convertiplanes" with rotors at the wing tips able to pivot between "helicopter mode" and "airplane mode," the most successful company in this arena has been Bell. Bell first explored the tiltrotor concept in the 1950s, but the idea did not attract military attention until the flight of the XV-15 research aircraft of the 1970s. This design, the first in which the entire rotor nacelle was pivoted, proved so successful that the Navy offered Bell and Boeing a contract to develop the concept into a transport aircraft for the Marine Corps. The resulting V-22 has a conventional cabin for two flight crew and up to 24 fully armed troops or cargo pallets. The two engine nacelles are located at each end of a slightly forward swept wing and are able to pivot through 97.5°. For greater safety, the engines are connected through a complex series of gearboxes so that one engine can power both nacelles in case the other engine fails. The V-22 also folds into a compact size for ship storage by folding the propeller blades inward and rotating the entire wing parallel to the fuselage. Due to its complexity and revolutionary design, the V-22 program has been plagued by technical difficulties, high cost, controversy, and the threat of cancellation. These issues were brought to a head in 2000 after two fatal accidents and revelations that Marine Corps officers had falsified maintenance records to improve the aircraft's readiness figures. These difficulties forced a two-year delay in the flight test program while the plane was grounded for modifications. After a nearly 20 year development period, however, the aircraft finally began entering service with the Marine Corps in 2007. Current plans call for the Marines to purchase 360 units of the MV-22. The Navy is to introduce 48 aircraft starting in 2008 while the Air Force will buy 50 CV-22 models with service entry slated for 2009. Last modified 26 October 2007
HISTORY:
First Flight	19 March 1989
Service Entry	June 2007
CREW:	three: pilot, co-pilot, loadmaster
PASSENGERS:	24 troops
ESTIMATED COST:	$69.9 million [2006$]
AIRFOIL SECTIONS:
Wing Root	Bell A821201 (23%)
Wing Tip	Bell A821201 (23%)
Rotor Blade Root	XN28/XN18/XN12
Rotor Blade Tip	XN09
DIMENSIONS:
Length	57.33 ft (17.47 m)
Wingspan	50.92 ft (15.52 m) including nacelles 84.50 ft (25.77 m) with rotors turning
Height	21.75 ft (6.63 m) with nacelles vertical
Rotor Diameter	38.00 ft (11.58 m) for each 3-bladed rotor
Wing Area	382 ft² (35.49 m²)
Rotor Disk Area	2,268 ft² (210.72 m²) total
Canard Area	not applicable
WEIGHTS:
Empty	33,140 lb (15,060 kg)
Normal Takeoff	47,500 lb (21,545 kg) [vertical TO]
Max Takeoff	52,870 lb (24,030 kg) [vertical TO] 57,000 lb (25,910 kg) [short TO, 20 deg tilt] 60,500 lb (27,500 kg) [short TO ferry]
Fuel Capacity	internal: 13,850 lb (6,295 kg) external: unknown
Max Payload	20,000 lb (9,090 kg) internally 15,000 lb (6,820 kg) externally 600 lb (272 kg) capacity rescue winch
PROPULSION:
Powerplant	two Rolls-Royce/Allison AE1107C turboshafts
Thrust	12,300 shp (9,172 kW)
PERFORMANCE:
Max Level Speed	at altitude: 390 mph (630 km/h) [airplane mode] at sea level: 115 mph (185 km/h) [helicopter mode]
Initial Climb Rate	2,320 ft (705 m) / min
Service Ceiling	25,000 ft (7,630 m)
Hover Ceiling (out of ground effect)	7,000 ft (2,135 m) [HV-22] 5,000 ft (1,525 m) [CV-22]
Range	typical: 505 nm (935 km) ferry: 2,100 nm (3,890 km)
g-Limits	unknown
ARMAMENT:
Gun	provision for two .50 caliber cabin guns
Stations	two external hardpoints
Air-to-Air Missile	none
Air-to-Surface Missile	none
Bomb	none
Other	none
KNOWN VARIANTS:
MV-22	Baseline assault transport for the US Marines, also equipped for medical evacutaion (up to 12 litters), search-and-rescue, supply transport, and special operations; 408 to be built
HV-22	Search-and-rescue model for the US Navy, also equipped for special operations duties and fleet logistics; 48 originally planned but this model was cancelled as the Navy will purchase the standard MV-22 variant instead
CV-22	Special operations model for the US Air Force, able to covertly insert and extract up to 18 troops while flying 500 nm (925 km) at 500 ft (150 m) or lower altitude; 50 to be built
PRV-22	Combat search-and-rescue model proposed to the US Air Force as a replacement for the HH-60G Pavehawk; not developed
KNOWN COMBAT RECORD:	Iraq - Operation Iraqi Freedom (USMC, 2007)
KNOWN OPERATORS:	United States (US Air Force) United States (US Marine Corps) United States (US Navy)
3-VIEW SCHEMATIC:
SOURCES: Donald, David, ed. The Complete Encyclopedia of World Aircraft. NY: Barnes & Noble, 1997, p. 118, Bell/Boeing V-22 Osprey. FAS V-22 site Gunston, Bill and Spick, Mike. Modern Fighting Helicopters. London: Salamander Books, 1998, p. 96-97, Bell/Boeing V-22 Osprey. _____. MV-22 Crash, Marine Corps Gazette, vol. 84, no. 5, May 2000, p. 10. Osprey On-Line US Navy V-22 Fact Sheet