
U.S. Navy Fact Sheet T-45A Goshawk training aircraft Description Features |
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| Point Of Contact Naval Air Systems Command Public Affairs Department 47123 Buse Road, Unit IPT Bldg. 2272, Suite 075 Patuxent River, MD 20670-5440 (301)757-1487 | ||
| General Characteristics | ||
| Primary Function: Training platform for Navy/Marine Corps pilots. | ||
| Contractor: Boeing Company. | ||
| Date Deployed: First flight, April 1988; Operational, 1991. | ||
| Unit Cost: $17.2 million. | ||
| Propulsion: Rolls Royce F405-RR-401 turbofan engine with 5,527 pounds thrust. | ||
| Length: 39 feet 4 inches (11.98 meters). | ||
| Height: 13 feet 6 inches (4.11 meters). | ||
| Wingspan: 30 feet 10 inches (9.39 meters). | ||
| Weight: Take-off maximum gross, 13,500 pounds (6,075 kg); empty 9,394 pounds (4,261 kg). | ||
| Airspeed: 645 miles per hour (1038 km per hour). | ||
| Ceiling: 42,500 feet. | ||
| Range: 700 nautical miles (805 statute miles, 1288 km). | ||
| Crew: Two (instructor pilot, student pilot). | ||
| Armament: None. | ||
| Last Update: 18 February 2009 | ||