Redirected from SCUD
All models are 11.25 meters long (except Scud-A, which is one meter shorter) and 0.88 meters in diameter. They are propelled by a single engine burning either kerosene and nitric acid in the Scud-A, or UDMH and RFNA (Russian SG-02 Tonka 250) in other models.
The name "Scud" is also used to refer to an Iraqi modification of the same missile. Altered for greater range, it came to particular prominence during the Gulf War, when a number of missiles were fired at Israel (40) and Saudi Arabia (46). The US-made Patriot missile system claimed successes in shooting down the missiles, but many critics claim that the accuracy of the Patriot missiles has been greatly exaggerated.
All "Scud" versions derive from the German V-2 rocket (just like the majority of early American missiles and rockets) and are (very) inaccurate due to their construction. The Iraqi modifications increased range, at the cost of accuracy.
As with some other missiles, the military advantage of this weapon consists in its ease of transportation, on a TEL vehicle (transporter-erector-launcher). This mobility allows for a choice of firing position and increases the survivability of the weapon system (to such an extent, that of the approximately 100 launchers claimed destroyed by coalition pilots and special forces in the Gulf War not a single destruction could be confirmed afterwards).
The Iraqis developed four versions: Scud, longer-range Scud, Al Hussein[?], and Al Abbas[?]. Apart from the almost unmodified weapon these were not successful missiles as they tended to break up in flight and had small warheads.
DIA | SS-1b | SS-1c | SS-1d | SS-1e |
NATO | Scud-A | Scud-B | Scud-C | Scud-D |
Deployment Date | 1957 | 1965 | 1965 | 1980s |
Withdrawn | 1978 | |||
Range | 130 km | 300 km | 575-600km | 700 km |
CEP (NATO estimate) | 4,000 m | 900 m | 900 m | 50 m |
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