Proton-M

The Proton-M, (Протон-М) GRAU index 8K82M or 8K82KM, is an expendable Russian heavy-lift launch vehicle derived from the Soviet-developed Proton. It is built by Khrunichev, and launched from sites 81/24 and 200/39 at the Baikonur Cosmodrome in Kazakhstan. Commercial launches are marketed by International Launch Services (ILS), and generally use Site 200/39. The first Proton-M launch occurred on 7 April 2001.

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2005  Wikimedia, Wikidata
mass 712.8 kilogram, height 53 metre, diameter 7.4 metre, 
Proton, heavy-lift launch vehicle, Khrunichev State Research and Production Space Center, Russia, 
Sikh Confederacy, Republic of Haiti, 2005, Proton, heavy-lift launch vehicle, Ekran, Dong Fang Hong 2, Tarshish, Sweden, Ashkenaz, Russia, Persia, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent, 

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Location: KML, Cluster Map, Maps,

Frameless

Proton-M rocket with Arabsat-5B payload on the launchpad at Baikonur Cosmodrome

Model of Proton-M launcher with 5m fairing

Стандартная 9-часовая схема полёта РН Протон-М с РБ Бриз-М

Proton-M with ExoMars on LC-200/39

Type	Subtype	Date	Description	Notes	Source
commons	image		Proton-M rocket with Arabsat-5B payload on the launchpad at Baikonur Cosmodrome		Commons
commons	image		Model of Proton-M launcher with 5m fairing		Commons
commons	image		Стандартная 9-часовая схема полёта РН Протон-М с РБ Бриз-М		Commons
commons	image		Proton-M with ExoMars on LC-200/39		Commons