Lockheed D-21

The Lockheed D-21 is an American supersonic reconnaissance drone. The D-21 was initially designed to be launched from the back of an M-21 carrier aircraft, a variant of the Lockheed A-12 aircraft. The drone had maximum speed in excess of Mach 3.3 (2,200 miles per hour; 3,600 kilometers per hour) at an operational altitude of 90,000 feet (27,000 meters). Development began in October 1962. Originally known by the Lockheed designation Q-12, the drone was intended for reconnaissance deep into enemy airspace. The D-21 was designed to carry a single high-resolution photographic camera over a preprogrammed path, then release the camera module into the air for retrieval, after which the drone would self-destruct. Following a fatal accident when launched from an M-21, the D-21 was modified to be launched from a Boeing B-52 Stratofortress. Several successful test flights were made, followed by at least four unsuccessful operational D-21 flights over China, before the program was canceled in 1971.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Lockheed Corporation
- Category
- Reconnaissance
- Country of origin
- United States
- First flight
- 1964-12-22
- Length
- 13.061 m
- Wingspan
- 5.814 m
Specifications
- Cruise speed
- 2,193 kt
- Max speed
- 2,884 kt
- Range
- 3,000 nm
- Service ceiling
- 95,000 ft
- Max takeoff weight
- 11,000 lb
- Powerplant
- Marquardt RJ43-MA-20S4
- Engines
- 1
- Length
- 42.8 ft
- Wingspan
- 19 ft
- Height
- 7 ft
- Number built
- 38
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.