Zond 3MV-1 No.2 explained

Zond 3MV-1 No.2
Mission Type:Venus flyby
Operator:OKB-1
Mission Duration:Launch failure
Cospar Id:1964-F01
Satcat:00277
Spacecraft Type:3MV-1
Launch Mass:800kg (1,800lb)[1]
Launch Date: UTC[2]
Launch Site:Baikonur 1/5
Programme:Venera
Previous Mission:Kosmos 21
Next Mission:Kosmos 27

Zond 3MV-1 No.2 (or No. 4A), also known as Venera 1964A in the West, was a Soviet spacecraft, which was launched in 1964 as part of the Zond program. Due to a problem with its carrier rocket third stage, it failed to reach low Earth orbit.[3]

Launch

Zond 3MV-1 No.2 was launched at 05:47:40 UTC on 19 February 1964, atop a Molniya 8K78M carrier rocket flying from Site 1/5 at the Baikonur Cosmodrome.[4] During ascent, LOX entered an RP-1 duct due to a leaking valve and formed a glob of explosive gel. When core separation and Blok I ignition began, the thrust section exploded. The remains of the stage and probe landed 52 miles (85 kilometers) north of the town of Barabinsk in Siberia.

See also

Notes and References

  1. Web site: Zond (3MV-1A #1, 2) . Krebs . Gunter . Gunter's Space Page . 15 July 2017.
  2. Book: Beyond Earth: A Chronicle of Deep Space Exploration, 1958–2016. 37–38. Siddiqi. Asif A.. 2017059404. 9781626830424. NASA History Program Office. second. 2018. SP2018-4041. The NASA history series. Washington, DC.
  3. Web site: Russia's unmanned missions to Venus . Zak . Anatoly . RussianSpaceWeb.com . 10 January 2011 . dead . https://web.archive.org/web/20110526053131/http://www.russianspaceweb.com/spacecraft_planetary_venus.html . 26 May 2011 .
  4. Web site: Launch Log . McDowell . Jonathan . Jonathan's Space Page . 10 January 2011.