UR-200
Sign in to saveAlso known as UR200, 8K81, SS-10 Scrag, Scrag Missile, SS10
The UR-200 was an intercontinental ballistic missile (ICBM) developed by Vladimir Chelomey's OKB-52 in the Soviet Union. It was known during the Cold War by the NATO reporting name 'SS-10 Scrag and internally by the GRAU index 8K81'. The design was authorized by the Decisions of the Central Committee of the CPSU of March 16 and August 1, 1961, and the draft project was finished in July 1962. It first flew on November 4, 1963, from the Baikonur Cosmodrome. The ninth and final flight was conducted on October 20, 1964.
Key facts
- Weapon.name
- UR-200SS-10 Scrag
- Weapon.image
- Side sketch of UR-200 ballistic missile.jpg
- Weapon.image_size
- 300
- Weapon.origin
- Soviet Union
- Weapon.type
- Intercontinental ballistic missile
- Weapon.is_missile
- yes
- Weapon.service
- 1963-1964
- Weapon.designer
- OKB-52
- Weapon.design_date
- 1962
- Weapon.spec_label
- 8K81
- Weapon.filling
- Nuclear warhead
- Weapon.engine
- First stage, RD-0202 liquid-fuel rocketSecond stage, RD-0205 liquid-fuel rocket
- Weapon.engine_power
- First stage, Second stage,
- Weapon.guidance
- Inertial
- Weapon.propellant
- / UDMH
- Weapon.ceiling
- apogee
via Wikipedia infobox
Wikidata facts
- Image
- Side sketch of UR-200 ballistic missile.jpg
Show 3 more facts
- NATO reporting name
- Scrag
- Commons category
- UR-200
- military designation
- SS-10
Sources (1)
via Wikidata · CC0
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Article
7 sectionsContents
- Description
- FOBS
- Operational history
- Operators
- Related developments
- See also
- References
The UR-200 was an intercontinental ballistic missile (ICBM) developed by Vladimir Chelomey's OKB-52 in the Soviet Union. It was known during the Cold War by the NATO reporting name 'SS-10 Scrag and internally by the GRAU index 8K81. The design was authorized by the Decisions of the Central Committee of the CPSU of March 16 and August 1, 1961, and the draft project was finished in July 1962. It first flew on November 4, 1963, from the Baikonur Cosmodrome. The ninth and final flight was conducted on October 20, 1964.
==Description== The UR-200' was a two-stage liquid-propellant universal ICBM for delivery of replaceable payloads to the range up to 12000 km, launch of interceptor satellites for space defense, naval recon satellites, and orbital maneuvering warheads. It was capable of carrying around of payload, and could be launched from flat pads, or missile silos built for the R-16 missile. Unusually for a Soviet missile, the first stage provided attitude control by means of thrust vectoring. Nitrogen tetroxide and UDMH were used as propellants.