Scud missile

Scud is the NATO reporting name (not an acronym) for a Russian army short-range liquid propellant surface-to-surface ballistic missile, the SS-1. The Makeyev OKB Design Bureau developed it from the German V2 in the 1950s. Variants were the -B in 1961 and the -C in 1965, both of which could carry either a conventional high-explosive, a 5-80 kiloton nuclear, or a chemical (thickened VX) warhead. The -D variant developed in the 1980s can deliver can carry a conventional high-explosive warhead, a fuel-air warhead, 40 runway-penetrator sub-munitions, or 100 5-kg anti-personnel bomblets.

All models are 11.25 meters long (except Scud-A, which is one meter shorter) and 0.88 meter 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 missles has been greatly exaggerated.

As with some other missiles, the military advantage of this weapon is that is it is easily transported, for example on a launching vehicle like a truck.

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.

General Characteristics

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Withdrawn	1978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