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  2. R-1 (missile) - Wikipedia

    en.wikipedia.org/wiki/R-1_(missile)

    The R-1 rocket (NATO reporting name SS-1 Scunner, Soviet code name SA11, GRAU index 8A11) was a tactical ballistic missile, the first manufactured in the Soviet Union, and closely based on the German V-2 rocket. [2] The R-1 missile system entered into service in the Soviet Army on 28 November 1950.

  3. Soviet rocketry - Wikipedia

    en.wikipedia.org/wiki/Soviet_rocketry

    The R-7 Rocket was a Soviet missile developed during the Cold War as the R-7 Semyorka (Russian: Р-7 Семёрка). It was the world's first intercontinental ballistic missile , launched Sputnik 1 , the first artificial satellite, into orbit, and became the basis for the R-7 family which includes Sputnik , Luna , Molniya , Vostok , and ...

  4. N1 (rocket) - Wikipedia

    en.wikipedia.org/wiki/N1_(rocket)

    The N1 (from Ракета-носитель Raketa-nositel', "Carrier Rocket"; Cyrillic: Н1) [5] was a super heavy-lift launch vehicle intended to deliver payloads beyond low Earth orbit. The N1 was the Soviet counterpart to the US Saturn V and was intended to enable crewed travel to the Moon and beyond, [6] with studies beginning as early as ...

  5. Nedelin catastrophe - Wikipedia

    en.wikipedia.org/wiki/Nedelin_catastrophe

    The Nedelin catastrophe or Nedelin disaster, known in Russia as the Catastrophe at Baikonur Cosmodrome (Russian: Катастрофа на Байконуре, romanized: Katastrofa na Baikonure), was a launch pad accident that occurred on 24 October 1960 at the Baikonur Cosmodrome in Soviet Kazakhstan.

  6. German influence on Soviet rocketry - Wikipedia

    en.wikipedia.org/wiki/German_influence_on_Soviet...

    In early 1945 a team of Soviet rocket specialists were sent to Germany to identify and recover German rocket technology. [17] The first Soviet team to arrive at Nordhausen, the main V-2 construction site, were disappointed, United States teams had already removed approximately 100 completed V-2 missiles and destroyed what remained. In addition ...

  7. R-2 (missile) - Wikipedia

    en.wikipedia.org/wiki/R-2_(missile)

    Like its predecessor, the R-1, the R-2 was a single-stage missile using ethanol as a fuel and liquid oxygen as an oxidizer. [4]: 243 At a length of 17.65 m (57.9 ft) and a mass of 19,632 kg (43,281 lb), the R-2 was 2.5 m (8 ft 2 in) longer and the dry weight of 4,528 kg (9,983 lb) was about 500 kg (1,100 lb) heavier than the R-1. [7]

  8. Sergei Korolev - Wikipedia

    en.wikipedia.org/wiki/Sergei_Korolev

    Sergei Pavlovich Korolev [a] [b] [c] (12 January 1907 [O.S. 30 December 1906] – 14 January 1966) was the lead Soviet rocket engineer and spacecraft designer during the Space Race between the United States and the Soviet Union in the 1950s and 1960s.

  9. 1951 in spaceflight - Wikipedia

    en.wikipedia.org/wiki/1951_in_spaceflight

    The R-2 missile, the first operational Soviet design to have a separable nose cone, underwent a second test series of thirteen flights in July 1951, experiencing one failure. Accepted for operational service on 27 November 1951, [ 9 ] the design had a range of 600 kilometres (370 mi), twice that of the R-1, while maintaining a similar payload ...