RT-2PM2 Topol-M: Difference between revisions

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|engine=Three-stage [[Solid-fuel rocket]]
|engine_power=
|weight= 47{{convert|57,200 000|kg (104,000 lb)|abbr=on}}
|length={{convert|22.774|m|abbr=on}}
|height=
|diameter={{convert|12.9328|m|abbr=on}}
|wingspan=
|speed={{convert|7520|m/s|km/h mph Mach}}<ref name="Mputtre.com">{{cite web |url=http://www.mputtre.com/id19.html |title=Topol-M: Missile Defense Penetrator by Michal Fiszer |publisher=Mputtre.com |access-date=2011-05-23 |url-status=dead |archive-url=https://web.archive.org/web/20121230165047/http://www.mputtre.com/id19.html |archive-date=2012-12-30 }}</ref>
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|ceiling=
|altitude=
|filling= 1 x 1.03 [[Mt]] or 4 x 750 [[kt]] <ref name="sipri.org">[https://global.oup.com/academic/product/sipri-yearbook-online-2011-9780199695522?cc=us&lang=en& SIPRI Yearbook Online 2011]</ref>
|guidance=[[Inertial guidance system|Inertial]] with [[GLONASS]]<ref>{{cite web|url=http://missiledefenseadvocacy.org/missile-threat-and-proliferation/missile-proliferation/russia/ss-27-topol-m/|title=Missile Defense Advocacy Alliance » SS-27 / Topol-M|last=www.missiledefenseadvocacy.org|website=missiledefenseadvocacy.org}}</ref>
|accuracy=200 m [[Circular error probable|CEP]]<ref name="Mputtre.com"/>