MV-22 OspreyCountry of Origin: United StatesImages courtesy of the U.S. Department of Defense; click on image to display larger version |
Specifications | |
Type: Tilt-rotor VTOL-capable transport | Manufacturer: Boeing / Bell Helicopter Textron/td> |
Armor Material: Composites | Armor Thickness: n/a |
Length: 17.47 m | Width over propellers: 25.78 m |
Weight: 25,000 kg (max STOL takeoff wt) | Maximum Speed: 510 kph |
Powerplant: 2 x Rolls-Royce Liberty AE1107C turobshafts | Horsepower: 6,830 shp each |
Description | |
Size: 10 | Total Actions: 2 |
Offense |
None fitted as standard, but a rear-facing LMG or HMG is often fitted |
Defense | |
Primary Movement: Flight 0/15/17 (510 kph) | Secondary Movement: Ground 23/46 (258 kph, for STOL takeoff) |
Maneuver: -2 | Armor: 12 / 24 / 36 |
Miscellaneous | |
Crew: 3 (Pilot, Copilot, Crew Chief) | Deployment Range: 1630 km |
Sensors: +1 / 3 km ground, 30 km air | Communications: +1 / 20 km ground, 200 km air |
Perks: Airlift Winch (rescue hoist, AUX, Rating 2), Backup Communications, Cargo Bay (24.68 m3, max cargo weight: 9070 kg), Chaff/Flare Dispensers (AUX, Rating 2, 60 shots), NOE Flyer, Passenger Seating (24), Refueling Intake | Flaws: Difficult to Modify, Exposed Movement System, Fuel Inefficient (applies only to vertical takeoffs; if short takeoff is used, efficiency is normal), Large Sensor Profile (Rating 2), Maximum Ceiling (8000 m) |
Defects: None | Lemon Dice: 2 |