|
| General Information |
| Developed by |
France |
| Deployed by |
France, Argentina, Bahrain, Belgium, Brasil, Brunei, Cameroon, Chili, Colombia, Ecuador, Germany, Greece, Indonesia, Iraq, South Korea, Kuwait, Malaysia, Morocco, Nigeria, Oman, Pakistan, Peru, Philippines, Qatar, Saudi Arabia, Thailand, Tunisia, UAE, UK |
| Development Year |
1968 |
| Deployment Year |
1972 |
| Launcher |
aircraft pylon(AM39), launcher/container known as the VSM(SM39), tubular fiberglass container(MM40) |
| Number manufactured |
3,300 |
| Contractor |
MBDA |
| Dimensions and Performance |
|
Length |
4.69m(AM39), 4.69m(SM39), 5.80m(MM40) |
|
Body Diameter |
35cm, 35cm, 35cm |
|
Launch Weight |
670kg, 655kg, 870kg |
|
Range |
50-70km, 50km, 50-70km |
|
Speed |
Mach 0.93 |
|
Altitude |
9-15m(cruise), 8m(attack) |
| Components |
|
Propulsion |
2-stage solid propellant rocket |
|
Warhead |
165kg HE SAP |
|
Guidance |
inertial, active radar |
|