UR-200
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| UR-200 SS-10 Scrag | |
|---|---|
apogee | |
| Maximum speed | Mach 20 (24,500 km/h; 15,200 mph; 6.81 km/s) |
Guidance system | Inertial |
The UR-200 was an
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[clarification needed] 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
UDMH
were used as propellants.
FOBS
The FOBS, or
8K713 and R-36. The use of the UR-200 for FOBS deployment was cancelled in October 1964, when Nikita Khrushchev
was removed from power.
Operational history
The UR-200 was never deployed operationally. The successful development of the storable hypergolic-fuelled R-36 silo-launched missile led to the cancellation of the UR-200 in 1965.
Operators
Related developments
- R-9 Desna by Sergei Korolev
- R-16 by Mikhail Yangel
- Universal Rocket
- UR-100 "minor" missile in development set of UR-100..UR-200..UR-500 line
- UR-500"major" missile in development set of UR-100..UR-200..UR-500 line