AQM-81A Firebolt
The AQM-81A Firebolt is an unmanned high-altitude, supersonic aerial target powered by a “hybrid” rocket motor using a liquid oxidizer catalyst and solid propellant. Designed to permit USAF fighter pilots the opportunity to experience engaging a realistic air target, the Firebolt’s unique motor allows the in-flight adjustment of thrust to alter the UAV’s speed and altitude effectively simulating a high-performance aircraft.
Intended to be air-launched from a manned aircraft, the AQM-81A Firebolt is equipped with a Scalar Scoring System providing missile miss-distance information throughout a 150-foot sphere centered on the target. The vehicle contains a Mid-Air Retrieval System (MARS), a parachute recovery system and a floatation device to allow midair retrieval, land or water recovery.
Designated the Teledyne Ryan Model 305 the AQM-81A Firebolt was deemed too expensive and was never operationally produced.
This aircraft is on loan from the NMUSAF.
| Manufacturer: | Teledyne Ryan | ||
| Designation: | AQM-81A | ||
| Nickname: | Firebolt | ||
| Type: | Target Drone | ||
| Specifications | |||
|---|---|---|---|
| Length: | 17′ | ||
| Height: | 2′ 2″ | ||
| Diameter: | 1′ 1″ | ||
| Propulsion | |||
| No. of Engines: | 1 | ||
| Powerplant: | United Technology Chemical Systems Division Hybrid Rocket Motor | ||
| Performance | |||
| Endurance: | Mach 3 for 5 minutes | ||
| Max Speed: | Mach 4.3 (Approximately 2,600 mph) | ||
| Ceiling: | 100,000′ | ||