The AQM-60 Kingfisher, developed by the Lockheed Corporation, was a target version of the USAF's X-7 test aircraft. The X-7's development began in 1946 after a request from the USAF for a Mach 3 unmanned test vehicle. This unmanned test craft eventually evolved into the Kingfisher when the need arose for a target to test anti-missile systems such as the SAM-A-7/MIM-3 Nike Ajax, SAM-A-25/MIM-14 Nike Hercules, and IM-99/CIM-10. Unfortunately for the tests the Kingfisher proved a bit too elusive, managing to evade the vast majority of the anti-missile systems and only being shot down a few times during the tests. This, coupled with political fall-out from the program, led to the eventual discontinuation of production in 1959 and the cancellation of the project in the mid-1960s.
Specifications [edit]
General characteristics
- Length: 38 ft 1 in (11.6 m)
- Wingspan: 9 ft 10 in (3 m)
- Height: 6 ft 11 in (2.1 m)
- Gross weight: 7,937 lb (3,600 kg)
- Powerplant: 1 × Marquardt XRJ43-MA ramjet (Sustainer)
- Powerplant: 2 × Thiokol XM45 (5KS50000) solid-fuel rockets, 50,000 lbf (222 kN) thrust each for 5s (Boosters)
Performance
- Maximum speed: Mach 4.3
- Range: 113 nmi; 130 mi (210 km)
- Service ceiling: 98,000 ft (30,000 m)
References [edit]
|
|
|
Manufacturer
designations |
|
Basic Model
Numbers
|
|
|
|
Lockheed-California
Temporary Design
Numbers
|
|
|
|
| By role |
|
Airliners and
civil transports
|
|
|
|
Military transports
|
|
|
|
Attack and bombers
|
|
|
|
Drones/UAVs
|
|
|
|
EW and
reconnaissance
|
|
|
|
Fighters
|
|
|
|
Helicopters
|
|
|
|
Maritime patrol
|
|
|
|
Trainers
|
|
|
|
Experimental
|
|
|
|
| Names |
|
|
USAF drone aircraft designations 1948–1962
|
|
|
|
|
|
1 Not assigned
|
|
|
|
|
| General |
|
|
| Military |
|
|
| Accidents/incidents |
|
|
| Records |
|
|