Roland (missile)
| Roland | |
|---|---|
 |
|
| Type | Surface-to-air missile |
| Production history | |
| Manufacturer | Euromissile |
| Specifications | |
| Weight | 67 kg |
| Length | 2.40 m |
| Diameter | 16 cm |
| Warhead | 6.5 kg (14.3 lb) pre-fragmented high-explosive |
|
|
|
| Engine |
Dual-thrust solid-fueled rocket:
|
| Wingspan | 50 cm |
|
Operational
range |
8,000 m |
| Flight altitude | 5,500 m |
| Speed | Mach 1.6 |
|
Guidance
system |
tracking radar |
Dual-thrust solid-fueled rocket:
The Roland is a Franco-German mobile short-range surface-to-air missile (SAM) system. The Roland was also purchased by the U.S. Army as one of very few foreign SAM systems.
Roland was designed to a joint French and German requirement for a low-level mobile missile system to protect mobile field formations and fixed, high-value targets such as airfields. Development began in 1963 as a study by Nord Aviation of France and Bölkow of Germany with the system then called SABA in France and P-250 in Germany. The two companies formed a joint development project in 1964 and later (as Aérospatiale of France and MBB of Germany) founded the Euromissile company for this and other missile programs. Aerospatiale took primary responsibility for the Roland 1 day/clear-weather system while MBB took primary responsibility for the Roland 2 all-weather system. Aerospatiale was also responsible for the rear and propulsion system of the missile while MBB developed the front end of the missile with warhead and guidance systems. The first guided launch of a Roland prototype took place in June 1968, destroying a CT-20 target drone and fielding of production systems was expected from January 1970. The test and evaluation phase took much longer than originally anticipated with the clear-weather Roland I finally entering operational service with the French Army in April 1977, while the all-weather Roland II was first fielded by the German Army in 1978 followed by the French Army in 1981. The long delays and ever-increasing costs combined with inflation meant Roland was never procured in the numbers originally anticipated.
The Roland SAM system was designed to engage enemy air targets flying at speeds of up to Mach 1.3 at altitudes between 20 meters and 5,500 meters with a minimum effective range of 500 meters and a maximum of 6,300 meters. The system can operate in optical or radar mode and can switch between these modes during an engagement. A pulse-doppler search radar with a range of 15–18 km detects the target which can then be tracked either by the tracking radar or an optical tracker. The optical channel would normally be employed only in daylight against very low-level targets or in a heavy jamming environment.
The Roland missile is a two-stage solid propellant unit 2.4 meters long with a weight of 66.5 kg including the 6.5 kg multiple hollow-charge fragmentation warhead which contains 3.5 kg of explosive detonated by impact or proximity fuses. The 65 projectile charges have a lethal radius of 6 meters. Cruising speed is Mach 1.6. The missile is delivered in a sealed container which is also the launch tube. Each launcher carries two launch tubes with 8 more inside the vehicle or shelter with automatic reloading in 10 seconds.
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Wikipedia