
Specifications | ||
| Aerospatiale | ||
| Year | 1973 | |
|
In-service in the French Armed Forces : |
1985 (on Jaguar), 1993 (on Mirage 2000D), 1995 (on upgraded Super Etendard) |
|
| Type | short- to medium-range standoff missile | |
|
Typical mission |
Bombardment of targets requiring high precision |
|
| Modifications |
AS.30 - basic missile AS.30L - laser-guided version [Data for AS.30L] | |
| Wingspan | 1.0 m | |
| Length | 3.7 m | |
| Diameter | 0.34 m | |
| Launch weight | 520 kg | |
| Max. speed | 1700 km/h | |
| Ceiling | 10000 m | |
| Minimum range | 3 km | |
| Maximum range | 11 km | |
| Propulsion | two stage solid propellant rocket motors, composite booster, double-based sustainer | |
| Guidance | semi-active laser homing | |
| Warhead | impact-fuzed high-explosive semi-armor piercing, 240 kg Can pierce 2 meters of concrete before blowing up | |
|
Ignition : |
Impact fuse with possible retarded spark |
|
|
Special related equipment : |
Laser pod Atlis (Thomson-CSF) Laser designation pod with thermal camera (Thomson-CSF) |
|
|
Major operational capabilities : |
High accuracy on target (1m) with ground or airborne laser lightning (pod Atlis or PDL-CT) Success rate of 97% for about 60 missiles launched in the Gulf in 1991 and in Bosnia in 1995 |
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|
Number of units produced : |
More than 900 |
|
|
Possible carrying aircraft : |
Mirage 2000D, Mirage 2000-5, F 16, Jaguar, Mirage F1, upgraded Super Etendard, Rafale |
|
| Service | France, Great Britain, South Africa, Egypt, Iraq, Germany, Peru, Switzerland, India. | |
| Builder : | Thomson-CSF Optronique |
| In-service in the French Air Force : | 1993 (1999 for the PDL-CT S) |
| Length : | 2.85 m |
| Weight : | 340 kg |
| Related armament : | AS-30 laser ; 1,000-kg BGL ; GBU |
| Major operational capabilities : | Detection, target identification, night and day laser guidance of weapons |
| Number of units produced : | 50 planned for 2000 |
| Main user nations : | Italy, Saudi Arabia |
| Possible carrying aircraft : | Mirage 2000D, Tornado |