Q3071792: Difference between revisions
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Q3071792
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{{Page|Soyuz-2-1v|Classes|version of the Soyuz-2 rocket|14A15 | {{Page|Soyuz-2-1v|Classes|version of the Soyuz-2 rocket|14A15; Soyuz 2.1v; Soyuz-1; Soyuz-2-1V}} | ||
Latest revision as of 12:51, 2 September 2025
The Soyuz‑2.1v was a Russian expendable small-lift launch vehicle, developed as a derivative of the Soyuz-2 series. It is notable for omitting the four strap-on boosters common to other R-7 family rockets, making it the first R-7 variant without them.
2013 Website,
Wikimedia, Wikidata
14A15; Soyuz 2.1v; Soyuz-1; Soyuz-2-1V
mass 158000 kilogram, height 44 metre, diameter 3 metre,
Progress State Research and Production Rocket Space Center, Russia,
Russia, Progress State Research and Production Rocket Space Center, Dong Fang Hong 2, Ekran, Soyuz-2, 2013, 2010s,
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Location: KML, Cluster Map, Maps,
Gabinio.Soffitto Nella Casa Del Vescovo. Torino-Casa Del Vescovo Ovvero Casa Provana, Via Della Basilica 20, Interno, Particola 14A15
Воздушно-космические силы провели успешный пуск новой ракеты-носителя «Союз-2.1В» с космодрома Плесецк 04
Воздушно-космические силы провели успешный пуск новой ракеты-носителя «Союз-2.1В» с космодрома Плесецк 02
Воздушно-космические силы провели успешный пуск новой ракеты-носителя «Союз-2.1В» с космодрома Плесецк 06



