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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. 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 ...

  4. 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 ...

  5. 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 ...

  6. R-16 (missile) - Wikipedia

    en.wikipedia.org/wiki/R-16_(missile)

    Even when fueled and in an alert posture, the Soviet missiles still needed to wait up to twenty minutes to spin up the gyroscopes in their guidance systems before launch was possible. Despite these shortcomings, the R-16 was unquestionably the first truly successful intercontinental ballistic missile developed by the Soviet Union.

  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. R-12 Dvina - Wikipedia

    en.wikipedia.org/wiki/R-12_Dvina

    The R-12 is a single-stage rocket with a separable single reentry vehicle. In the integrated fuel tanks the oxidizer was put forward of the fuel tank, separated by an intermediate plate. During flight this allowed the oxidizer from the lower unit to be spent first, improving in-flight stabilization.

  9. R-27 (air-to-air missile) - Wikipedia

    en.wikipedia.org/wiki/R-27_(air-to-air_missile)

    R-27T. The Vympel R-27 (NATO reporting name AA-10 Alamo) is a family of air-to-air missiles developed by the Soviet Union during the late Cold War-era.It remains in service with the Russian Aerospace Forces, air forces of the Commonwealth of Independent States and air forces of many other countries as the standard medium-range air-to-air missile despite the development of the more advanced R-77.