AGM-76 Falcon
| AGM-76 Falcon | |
|---|---|
 Aerodynamic test model of the AGM-76A on display at the Steven F. Udvar-Hazy Center | |
| Type | Anti-radiation missile |
| Place of origin | United States |
| Service history | |
| Used by | United States Air Force |
| Production history | |
| Designed | 1966 |
| Manufacturer | Hughes Aerospace |
| Specifications | |
| Weight | 951 pounds (431 kg) |
| Length | 13 feet 4 inches (4.06 m) |
| Diameter | 13.5 inches (340 mm) |
| Warhead | high explosive |
| Warhead weight | 250 pounds (110 kg) |
|
| |
| Engine | Lockheed XSR13-LP-1 |
| Propellant | Solid fuel |
| Speed | Mach 4 |
Guidance system | Passive radar homing |
Launch platform | F-4D, A-6B, F-105F |
The AGM-76 Falcon was an air-to-surface anti-radiation missile developed by the United States Air Force during the Vietnam War. Intended as a conversion using off-the-shelf parts, it did not go into operational service.
Overview
During 1966, the United States Air Force began development of a heavy anti-radiation missile for use against surface-to-air missile radars in Vietnam. Using existing airframes from the cancelled AIM-47 Falcon heavy air-to-air missile project combined with the seeker head of the AGM-45 Shrike anti-radiation missile, the AGM-76A was fitted with a 250 pounds (110 kg) warhead of the type used in the Mark 81 bomb. Test-firings of AGM-76As were conducted from McDonnell F-4D Phantom II, Republic F-105F Thunderchief, and US Navy Grumman A-6B Intruder aircraft, however the missile was not put into production, the AGM-45 and AGM-78 Standard ARM becoming the standard anti-radiation missiles used by the United States.[1]
Operators
References
- ↑ Parsch, Andreas (19 January 2008). "Hughes AGM-76 Falcon". Directory of U.S. Military Rockets and Missiles. Designation-Systems. Retrieved 2017-11-25.