Sikorsky / Boeing RAH-66 Comanche
Reconnaissance / Attack Helicopter
The RAH-66 Comanche is a twin-engined two-seat advanced reconnaissance and attack helicopter developed by a joint venture between the American companies Boeing Helicopters and Sikorsky Aircraft. The RAH-66 Comanche was designed as a stealth helicopter with reduced Radar cross-section (RCS).
The RAH-66 Comanche program was cancelled by the US Army in 2004.
Propulsion | 2 Turboshaft Engines |
Engine Model | LHTEC T800-LHT-800 |
Engine Power (each) | 1166 kW | 1563 shp |
Speed | 328 km/h | 177 kts 204 mph |
Service Ceiling | 4.572 m | 15.000 ft |
Range | 485 km | 262 NM 302 mi. |
Empty Weight | 4.218 kg | 9.300 lbs |
max. Takeoff Weight | 5.597 kg | 12.339 lbs |
Rotor Blades (main/tail) | 5/Fenestron |
Main Rotor Diameter | 11,90 m | 39 ft 1 in |
Tail Rotor Diameter | 1,37 m | 4 ft 6 in |
Rotor Disc Area | 111,2 m² | 1197 ft² |
Length (Fuselage) | 13,22 m | 43 ft 4 in |
Length | 14,28 m | 46 ft 10 in |
Height | 3,37 m | 11 ft 1 in |
First Flight | 04.01.1996 |
Production Status | no mass production |
Total Production | 2 |
ICAO Code | H66 |
Data for (Version) | Sikorsky/Boeing RAH-66 Comanche |