Encyclopedia Astronautica
Mars 2MV-2



mars1.jpg
Mars 1 / 2MV-4
Mars 2MV-4. Other spacecraft in the 2MV series were similar.
Credit: NASA
Russian Venus probe. One launch, 1962.09.12, Sputnik 21.

Gross mass: 6,490 kg (14,300 lb).
First Launch: 1962.09.12.
Number: 1 .

More... - Chronology...


Associated Countries
See also
  • Soyuz The Russian Soyuz spacecraft has been the longest-lived, most adaptable, and most successful manned spacecraft design. In production for fifty years, more than 240 have been built and flown on a wide range of missions. The design will remain in use with the international space station well into the 21st century, providing the only manned access to the station after the retirement of the shuttle in 2011. More...

Associated Launch Vehicles
  • Soyuz Russian orbital launch vehicle. The world's first ICBM became the most often used and most reliable launch vehicle in history. The original core+four strap-on booster missile had a small third stage added to produce the Vostok launch vehicle, with a payload of 5 metric tons. Addition of a larger third stage produced the Voskhod/Soyuz vehicle, with a payload over 6 metric tons. Using this with a fourth stage, the resulting Molniya booster placed communications satellites and early lunar and planetary probes in higher energy trajectories. By the year 2000 over 1,628 had been launched with an unmatched success rate of 97.5% for production models. Improved models providing commercial launch services for international customers entered service in the new millenium, and a new launch pad at Kourou was to be inaugurated in 2009. It appeared that the R-7 could easily still be in service 70 years after its first launch. More...
  • Molniya 8K78 Russian orbital launch vehicle. Four stage derivative of the R-7 ICBM developed on a crash-program basis in 1960 for Soviet lunar and planetary deep space probe missions. The third stage found later use in the Voskhod and Soyuz launchers. By the 1970's mature versions of the launch vehicle were used almost entirely for launch of Molniya communications satellites and Oko missile early warning spacecraft into elliptical, 12-hour earth orbits. More...

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

Associated Programs
  • Venera Russian series of spacecraft that explored the planet Venus. Venera spacecraft made the first soft landings on the surface of Venus and returned the first images from the surface. More...

Bibliography
  • McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: here.
  • JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. Web Address when accessed: here.
  • Varfolomyev, Timothy, "Soviet Rocketry that Conquered Space - Part 5", Spaceflight, 1998, Volume 40, page 85.
  • "Otmenenniy Start "Molniya-M"", Novosti Kosmonavtiki, 1997, Issue 1, page 29.
  • Kamanin, N P, Skritiy kosmos, Infortext, Moscow, 1995.

Associated Launch Sites
  • Baikonur Russia's largest cosmodrome, the only one used for manned launches and with facilities for the larger Proton, N1, and Energia launch vehicles. The spaceport ended up on foreign soil after the break-up of Soviet Union. The official designations NIIP-5 and GIK-5 are used in official Soviet histories. It was also universally referred to as Tyuratam by both Soviet military staff and engineers, and the US intelligence agencies. Since the dissolution of the Soviet Union the Russian Federation has insisted on continued use of the old Soviet 'public' name of Baikonur. In its Kazakh (Kazak) version this is rendered Baykonur. More...

Mars 2MV-2 Chronology


1961 January 18 - . LV Family: R-7. Launch Vehicle: Molniya 8K78.
  • Venera preparations - . Nation: USSR. Spacecraft: Mars 2MV-2. The VVS contingent arrives at Tyuratam at 23:45 aboard an Il-14 for the Venera launch. Chertok is in charge of launch preparations. Due to various radio system problems, there can be no launch until 26 January. The death of Nedelin and the others still hangs over the cosmodrome.

1961 January 20 - . LV Family: R-9; R-7.
  • Venera preparations - . Nation: USSR. Related Persons: Korolev. Spacecraft: Mars 2MV-2; Vostok. Korolev plans three launches between 20 January and 14 February, but clearly his teams are not ready to accomplish this. There was insufficient testing of the Object V Venera spacecraft before it was shipped from OKB-1 to the cosmodrome. OKB-1 is trying to finish Object V on site, at the same time preparing the next Vostok 3KA and an R-9 ICBM for launch. Object V is not ready, the ability of its systems to function at long ranges and periods of time on the voyage to Venus are suspect. In Kamanin's opinion, it is diverting the crews from the higher priority manned and military projects.

1961 January 26 - . LV Family: R-16; R-7.
  • Venera delays - . Nation: USSR. Related Persons: Yangel. Spacecraft: Mars 2MV-2. Summary: The Object V launch is delayed to 1 February. Yangel has also had to postpone the next R-16 launch attempt to 26-30 January..

1961 January 31 - . LV Family: R-16; R-7.
  • Back at Tyuratam - . Nation: USSR. Related Persons: Korolev; Keldysh; Moskalenko; Semenov; Yangel. Spacecraft: Mars 2MV-2. Summary: Kamanin flies to the cosmodrome with Korolev, Keldysh, Moskalenko, General Semenov, and others. Yangel's R-16 ICBM is not ready for launch yet due to continuing problems with the radio systems. The Venera is set for a 2 February launch attempt..

1961 February 1 - . LV Family: R-7. Launch Vehicle: Molniya 8K78.
  • Venera rolled out to pad - . Nation: USSR. Spacecraft: Mars 2MV-2. Summary: The booster is 5 to 7 m taller than the Vostok. One gyroscope has to be replaced on the pad. Fuelling begins at 23:30. At 02:00 the launch is scrubbed due to continuing gyro problems. Next attempt is set for 4 February..

1962 September 12 - . 00:59 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Molniya 8K78. LV Configuration: Molniya 8K78 T103-14. FAILURE: At T+531 sec, the fourth vernier chamber of Stage 3's 8D715K engine exploded because the LOX cut-off valve had not closed as scheduled and LOX flowed into the hot chamber.. Failed Stage: 3.
  • Sputnik 21 - . Payload: 2MV-2 s/n 1. Mass: 6,500 kg (14,300 lb). Nation: USSR. Agency: RVSN. Program: Venera. Class: Venus. Type: Venus probe. Spacecraft: Mars 2MV-2. Decay Date: 1962-09-14 . USAF Sat Cat: 389 . COSPAR: 1962-A-Phi-1. Apogee: 218 km (135 mi). Perigee: 179 km (111 mi). Inclination: 64.9000 deg. Period: 88.40 min. Summary: The escape stage entered parking orbit but the main engine cut off just 0.8 s after ignition due to cavitation in the oxidiser pump and pump failure..

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