BQM-34A Firebee
The BQM-34A Firebee is a target drone developed by the American firm Teledyne Ryan Aeronautical. This UAV was built to satisfy the US Air Force’s need for a variable-speed target, essential for training fighter pilots and air defense crews.
Operational Deployment
The UAV was launched from the ground and subsequently controlled by an operator via radio. After being hit by a missile or completing its mission, the aircraft would descend by parachute. The prototype XQ-2 made its first flight in 1958, and the UAV entered service with the US Air Force in 1960.
Specialized Variants
The BQM-34S was a BQM-34A variant for the US Navy, featuring improved avionics. These included the AN/USW-4(V) ITCS (Integrated Tracking and Control System), AN/DKW-1 guidance transponders (later AN/DKW-2/-3B), and an A/A37G-8A flight control system. It was also equipped with a turbojet engine providing 871 kgf (8.67 kN) of thrust.
The MQM-34D, an Army variant of the BQM-34A with a ground launcher, was also produced.
Technical Specifications
| Modification | BQM-34A |
| Wingspan, m | 3.93 |
| Length, m | 6.99 |
| Height, m | 2.00 |
| Mass, kg | 935 |
| Engine type | 1 Continental J69-T-29 Turbojet |
| Thrust, kgf | 1 x 771 |
| Maximum speed, km/h | 933 |
| Stall speed, km/h | 327 |
| Practical range, km | 966 |
| Practical ceiling, m | 15636 |
Image and diagram gallery of the BQM-34A Firebee
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ArchivoAéreo Editorial Team
A group of aviation researchers and enthusiasts dedicated to documenting and preserving global aeronautical history. All articles are reviewed to ensure historical accuracy.
Sources & Accuracy
The information presented in this technical sheet has been compiled from declassified flight manuals, historical archives, and specialized literature. While we strive for maximum accuracy, some performance data may vary depending on the specific variant or operational conditions.