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Weapons of Mass Destruction (WMD)


R-11 / SS-1B SCUD-A
R-300 9K72 Elbrus / SS-1C SCUD-B

Specifications
DIA SS-1b SS-1c SS-1d SS-1e
NATO Scud-A Scud-B Scud-C Scud-D
Bilateral
Service R-11 / R-175 R-300
OKB/Industry 8K14
Design Bureau Makeyev OKB Makeyev OKB Makeyev OKB Makeyev OKB
Approved ............
Years of R&D ............
Engineering and Testing ............
First Flight Test ............
IOC ............
Deployment Date 1957196519651980s
Withdrawn1978
Type of Warhead
  • nuclear
  • Conventional unitary blast
  • Chemical warhead
  • HE, CHEM (thickened VX)
  • Conventional unitary blast
  • fuel-air explosive
  • 40 runway-penetrator sub-munitions
  • 100 11-lb (5-kg) anti-personnel bomblets
  • Warheads 1111
    Yield...5-80 kiloton ......
    Payload (t)770-950 kg
    Total length (m)10.25 m11.25 m11.25 m11.25 m
    Total length w/o warhead (m)
    Missile Diameter (m) 0.88 m0.88 m0.88 m0.88 m
    Launch Weight (t) 6,300 kg
    Fuel Weight (t)
    Range(km) 130 km300 km575-600km700 km
    CEP (m) (Russian Sources)
    CEP (m) (Western Sources)4,000 m900 m900 m50 m
    Reaction time 60 min
    Engine Designation ............
    Design Bureau ............
    Engine Configuration One engine One engine One engine One engine
    Propellants Liquid Storable Liquid Storable Liquid Storable Liquid Storable
    Fuel Kerosene UDMH UDMH UDMH
    Oxidizer nitric acid RFNA (Russian SG-02 Tonka 250)RFNA (Russian SG-02 Tonka 250)RFNA (Russian SG-02 Tonka 250)
    Main Engines Burning time (sec.) ............
    Main engines Thrust Sea Level/Vacuum (Tonnes) ............
    Main Engines Specific Impulse Sea Level/Vacuum (sec.) ............




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