ADAC: Difference between revisions
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Latest revision as of 18:05, 10 March 2019
Tracked Missile Air Defense Air Défense Antimissile Chenilles | |
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File:Amx45crotale.png | |
Type | Transporter Erector Launcher and Radar (TELAR) |
Place of origin | Sieuxerr |
Service history | |
In service | 1991 - Present |
Used by | Sieuxerr |
Production history | |
Designer | GIAT Industries Thomson-CSF |
Designed | 1985 |
Manufacturer | GIAT Industries (Now Nexter) Thomson-CSF (Now Thales) |
Produced | 1991 - Present |
Variants | See variants |
Specifications (ADAC Mk. III) | |
Weight | 36.5 tonnes |
Length | 6.8 m |
Width | 3.3 m |
Height | 3.5 m |
Crew | 3 (Commander, gunner, driver) |
Armor | Laminated steel/ceramic/composite mixture along with modular armor packages |
Main armament | 2 x 6 surface-to-air missiles |
Secondary armament | AA-77C (600 rounds) |
Engine | 8-cylinder diesel engine 850 horsepower (633 kW) |
Power/weight | 21.8 hp/t (16 kW/t) |
Transmission | SCT 2000 |
Suspension | torsion bar |
Ground clearance | .4 meters |
Fuel capacity | 1,300 ℓ |
Operational range | 550 km |
Speed | 70 km/h |
The ADAC is a tracked surface to air missile launching system. Capable of using a variety of air defense missiles with just modifications to software. In Sieuxerrian service, it used both the Roland 2/3 until the early 2000s, and the Crotale missiles.