Encyclopedia Astronautica
Mars 2MV-3

Mars 1 / 2MV-4
Mars 2MV-4. Other spacecraft in the 2MV series were similar.
Credit: NASA
Russian Venus probe. One launch, 1962.11.04, Sputnik 24. Mars probe intended to make a soft landing on Mars.

Gross mass: 890 kg (1,960 lb).
First Launch: 1962.11.04.
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
  • Mars Soviet Mars probes were intended to photograph Mars on flyby trajectories, followed by Mars orbit, landing, and Phobos reconnaisance missions. Essentially all of the series failed. More...

  • 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.
  • "Na Mars!", Novosti Kosmonavtiki, 1996, Issue 20, page 53.
  • National Space Science Center Planetary Page, As of 19 February 1999.. Web Address when accessed: here.

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-3 Chronology

1962 November 4 - . 15:35 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Molniya 8K78. LV Configuration: Molniya 8K78 T103-17. FAILURE: After T+260 sec, a malfunction of the pressurization system of the central sustainer led to cavitation in the oxidizer pipeline and LOX pump, followed at T+292s by the fuel pump.. Failed Stage: 1.
  • Sputnik 24 - . Payload: 2MV-3 s/n 1. Mass: 890 kg (1,960 lb). Nation: USSR. Agency: RVSN. Program: Mars. Class: Venus. Type: Venus probe. Spacecraft: Mars 2MV-3. Decay Date: 1962-11-05 . USAF Sat Cat: 451 . COSPAR: 1962-B-Xi-1. Apogee: 170 km (100 mi). Perigee: 170 km (100 mi). Inclination: 64.8000 deg. Period: 87.90 min. Mars probe intended to make a soft landing on Mars. Although the escape stage and payload reached orbit, the strong third stage vibrations shook a fuse loose from its mount in the main nozzle of the escape stage Block L's engine. The engine could not be ignited and remained in Earth orbit. It decayed about two months after insertion.

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