
| RAH-66 Comanche Specifications |
| Primary Function: | Scout Helicopter | | Contractor: | Boeing Helicopter Company and Sikorsky Aircraft Division (joint venture) | | Crew: | Two | | Unit Cost: | N/A | | Powerplant | | | Two T800 1,440 SHP gas turbine engines 5-blade main rotor Fantail anti-torque | | Dimensions | | Length: | 46.78 feet (rotor turning) | | Width: | 39.04 feet (rotor turning) | | Height: | 11.0 feet (overall) | | Weights | | Empty: | 7,765 pounds | | Combat Mission: | 10,600 pounds | | Performance | | Speed: | 330 km/hr / 172 knots - Dash speed 310 km/hr / 161 knots - Cruise speed | | Ceiling: | N/A | | Range: | 262 nm Max Range (internal fuel) 1,260 nm self-deployment range | | Armament | | | Air-to-air Stinger Hellfire 20mm three-barrel turreted gun Hydra-70 rockets | |
RAH-66 Comanche Achievements - The Comanche is the first helicopter developed specifically for armed reconnaissance.
RAH-66 Comanche Background The Comanche is a twin-turbine, two-seat (tandem) armed reconnaissance helicopter with projected missions of armed reconnaissance, light attack and air combat. Initial operating capability is set for the year 2006. It will replace obsolete AH-1 and OH-58 attack and observation helicopters. The RAH-66 incorporates stealth technology by housing all weapons inside weapons bays on the sides of the helicopter. The first RAH-66 took its first flight on January 4, 1996 at West Palm Beach in Florida.
RAH-66 Comanche Photos
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