
U.S. Navy Fact Sheet HH/UH-1N Iroquois helicopter Description Background |
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| Service Navy and Marine Corps | ||
| Point Of Contact Naval Air Systems Command Public Affairs Department 47123 Buse Road, Unit IPT Bldg. 2272, Suite 075 Patuxent River, MD 20670-5440 U.S. Marine Corps Headquarters Division of Public Affairs Washington, DC 20380-1775 | ||
| General Characteristics | ||
| Primary Function: Utility and transport helicopter. | ||
| Contractor: Bell Helicopter Company. | ||
| Date Deployed: Introduction date: January 1971. | ||
| Propulsion: Two Pratt and Whitney T400-CP-400 turboshaft engines; 1,250 hp (932 kw). | ||
| Length: 57 feet, 0 inches (17 meters). | ||
| Height: 14 feet 5 inches (4.4 meters). | ||
| Rotor Diameter: 48 feet (14.6 meters) with rotors spread. | ||
| Weight: Empty: 6,000 pounds (2,721.5 kg); Maximum Takeoff Weight: 10,500 pounds (4,762.7 kg). | ||
| Airspeed: Max cruise speed is 110 kts (203.7 km/hr). | ||
| Ceiling: 17,300 feet (5,273 meters). | ||
| Range: 286 miles (460 km). | ||
| Crew: Pilot, copilot, crew chief, gunner, plus 6 to 8 combat-equipped troops. | ||
| Last Update: 18 February 2009 | ||