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The '''RD-250''' ([[GRAU]] Index '''8D518''') is the base version of a dual-nozzle family of [[liquid-fuel rocket|liquid]] [[rocket engine
==Versions==
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* '''RD-251M''' ([[GRAU]] Index '''8D723M'''): A module comprising three RD-250M. Propulsion module of the [[R-36 (missile)|R-36-O]] (8K69) and [[Tsyklon-2]] first stage.
* '''RD-261''' ([[GRAU]] Index '''11D69'''): A module comprising three RD-250PM. Propulsion module of the [[Tsyklon-3]] first stage.<ref name=ea-rd261 />
== Comparison ==
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== Possible technological transfer to North Korea ==
Several experts think that technology from the RD-250 engine could have been transferred to North Korea (from Ukraine). This transfer would explain the rapid progress of North Korea in the development of two new missiles: the [[Intermediate-range ballistic missile|intermediate-range]] [[Hwasong-12]] and the [[intercontinental ballistic missile]] (ICBM), [[Hwasong-14]]. Due to complexity of the technology involved in this type of engine, modifications or reverse engineering seem difficult to achieve. Thus it's believable that complete hardware could have been bought on black market and directly shipped to North Korea, by Russia or Ukraine.<ref>{{Cite web|url=http://www.iiss.org/en/iiss%20voices/blogsections/iiss-voices-2017-adeb/august-2b48/north-korea-icbm-success-3abb|title=The secret to North Korea’s ICBM success|website=www.iiss.org|language=en|access-date=2017-08-15}}</ref>
==See also==
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