Encyclopedia Astronautica
R-5B


Russian intermediate range ballistic missile.

Gross mass: 24,400 kg (53,700 lb).
Height: 20.70 m (67.90 ft).
Diameter: 1.66 m (5.44 ft).
Thrust: 430.00 kN (96,660 lbf).
Apogee: 300 km (180 mi).
First Launch: 1962.10.18.
Last Launch: 1965.10.01.
Number: 7 .

More... - Chronology...


Associated Countries
See also
  • Early Russian Ballistic Missiles The true configuration of the world's first ICBM, the R-7, was revealed only in 1967, ten years after its first test. The Soviet N1 moon rocket was only revealed in 1990, 21 years after its first launch. At the same time, other Russian ballistic missiles were routinely paraded before the cameras of the world press even before they went into service. The extraordinary sensitivity of the Soviet leadership over these Korolev designs may be traced to the fact that they derived from the work of the Groettrup German rocket engineering team. More...
  • R-5 The R-5 was the first Soviet missile to be armed with a nuclear warhead, and the first for which the new southern facility at Dnepropetrovsk took over full design and production responsibility. The R-5 could deliver a 1425 kg warhead over a range of 1200 km, doubling the performance of the R-2. It was also the end of the road in being the ultimate extrapolation of German V-2 technology. Later missiles of both Yangel and Korolev would use other propellants and engine designs. More...
  • missile Guided self-propelled military weapon (as opposed to rocket, an unguided self-propelled weapon). More...

Associated Manufacturers and Agencies
  • Korolev Russian manufacturer of rockets, spacecraft, and rocket engines. Korolev Design Bureau, Kaliningrad, Russia. More...

Associated Launch Sites
  • Kapustin Yar Russia's first missile test range and used for satellite launches of smaller Kosmos vehicles. V-2's launched from here in 1946 were the first ballistic missiles fired on Soviet territory. It was greatly expanded as the test site for innumerable Soviet intermediate and short range missile projects in the 1950's.. Kapustin Year was also headquarters of the first operational R-1/R-2 units, 1950-1953, and later a base for 12 operational R-14 missile launchers. Kapustin Yar was known to have been used for over 3519 major launches from 1946 to 2007. More...
  • Kapustin Yar V-2 V-2, RT-15, R-5, R-2, R-17, R-11, R-1, Pioner, MR-12, M-100, Kosmos 3, Kosmos 2, RT-1, R-13, MMR-06, MERA launch complex. V-2 Launch Area More...

Associated Stages
  • R-5 Lox/Alcohol propellant rocket stage. Loaded/empty mass 27,250/3,250 kg. Thrust 479.22 kN. Vacuum specific impulse 244 seconds. More...

R-5B Chronology


1962 October 18 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5B.
  • Ionosphere mission - . Nation: USSR. Agency: AN. Apogee: 508 km (315 mi).

1962 October 22 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5B.
  • Aeronomy mission - . Nation: USSR. Agency: AN. Apogee: 500 km (310 mi).

1963 June 6 - . 00:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5B.
  • VAO Ionosphere / plasma mission - . Nation: USSR. Agency: AN. Apogee: 500 km (310 mi).

1963 June 18 - . 00:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5B.
  • VAO Aeronomy / ionosphere mission - . Nation: USSR. Agency: AN. Apogee: 500 km (310 mi).

1963 October 25 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5B.
  • VAO Aeronomy mission - . Nation: USSR. Agency: AN. Apogee: 500 km (310 mi).

1963 December 24 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5B.
  • VAO Aeronomy mission - . Nation: USSR. Agency: AN. Apogee: 500 km (310 mi).

1965 October 1 - . 03:57 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5B.
  • Ionosphere / solar x-rays mission - . Nation: USSR. Agency: AN. Apogee: 480 km (290 mi).

Home - Browse - Contact
© / Conditions for Use