Especificaciones
|
| TIPO |
misil guiado aire-superficie |
| Fabricantes |
Hughes Aircraft Co., Raytheon Co. |
| Planta Motriz |
Thiokol TX-481 motor cohete de propelente
solido |
| Autopiloto |
Navegacion inercial |
| Versiones |
AGM-65A/B |
AGM-65D |
AGM-65G |
AGM-65E |
AGM-65F |
| Servicio |
Air Force |
Marine Corps |
Navy |
| Peso en lanzamiento |
462 lbs
(207.90 kg) |
485 lbs
(218.25 kg) |
670 lbs
(301.50 kg) |
630 lbs
(286 kg) |
670 lbs
(301.50 kg) |
| Diametro |
1 foot (30.48 centimeters) |
| Envergadura |
2 feet, 4 inches (71.12 centimeters) |
| Alcance |
17+ miles (12 nautical miles/27 km) |
| Velocidad |
1150 km/h |
| Guia |
electro-optical television |
imagen infrarroja |
Laser |
buscador infrarrojo |
| Cabeza de guerra |
125 pounds
(56.25 kilogramos) |
300 pounds
(135 kilograms)
fusible de retardo |
125 pounds
(56.25 kilogramos) |
300 pounds
(135 kilograms)
fusible de retardo |
| Costo unitario |
|
$129,322 |
$158,688 |
| Despliegue |
August 1972 |
February 1986 |
1989 |
|
| Cantidad |
12,559 |
23,689 |
4,115 |
| Plataformas |
A-10,
F-15E
and
F-16 |
F/A-18 |
F/A-18 and AV-8B |