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Mission record

Venera 13

Also known as Venera 13 Flight Platform, Venera13

U.S.S.R · Launched

Explore trajectory

Completed · Success

One of a pair of identical Soviet spacecraft built to take advantage of the 1981 Venus launch opportunity and launched five days apart, each consisting of a flyby carrier bus and an attached descent craft. The descent craft plunged into the Venus atmosphere in March 1982, deployed a parachute at about 63 km altitude, released it at 47 km and used simple airbraking the rest of the way to the surface. After landing it started an imaging panorama and a mechanical drilling arm obtained a surface sample for analysis in a hermetically sealed chamber; the lander survived for 127 minutes against a planned design life of 32 minutes, transmitting to the carrier bus, which relayed its data as it flew by Venus.

Destinations
Launch vehicle
Proton Booster Plus Upper Stage and Escape Stages
Launch site
Tyuratam (Baikonur Cosmodrome), U.S.S.R
Countries
Soviet Union
Mission types
Flyby, Lander

Chronology

Mission timeline

  1. Launch

    Launched on a Proton-K booster from Baikonur Cosmodrome

    The launch/orbital information page prints 1981-10-30T06:04:00Z, recorded at minute precision because it prints a whole minute with zero seconds, and both master catalog pages give the same time. The agencies value follows this record's own master catalog page, which prints Funding Agency Unknown (U.S.S.R); the descent craft page for the same mission prints Funding Agency Soviet Academy of Sciences (U.S.S.R), and the disagreement is recorded rather than resolved.

    Earth
  2. Milestone

    First mid-course correction

    Both pages record two mid-course corrections, on 10 November 1981 and 21 February 1982, each printed as a full date.

  3. Milestone

    Final mid-course correction before Venus

    Both pages record a correction on 21 February 1982, printed as a full date.

  4. Deployment

    Descent craft separates from the carrier bus

    The flight platform page records that the descent module separated on 27 February 1982, printed as a full date.

    Venus
  5. Landing

    Lands at 7.5 S, 303 E near Phoebe Regio

    The descent craft page records that the parachute was deployed at 63 km altitude, released at 47 km with simple airbraking the rest of the way, that the descent lasted about an hour, and that Venera 13 landed at 03:57:21 UT at 7.5 S, 303 E, just east of the eastern extension of an elevated region known as Phoebe Regio. Carried at day precision from the plunge into the Venus atmosphere on 1 March 1982, which both pages print as a full date, and from the Decay Date of 1982-03-01 on the descent craft's own launch/orbital information page: the sentence that prints 03:57:21 UT prints no date beside it.

    Venus
  6. Milestone

    First colour images returned from the surface of Venus

    The descent craft page states that Venera 13 returned the first color images of the surface of Venus, revealing an orange-brown flat bedrock surface covered with loose regolith and small flat thin angular rocks. The wording is quoted from NSSDCA rather than derived here. A mechanical drilling arm obtained a sample whose composition, determined by the X-ray fluorescence spectrometer, put it in the class of weakly differentiated melanocratic alkaline gabbroids, and the acoustic detector returned the sounds of the spacecraft operations and the background wind.

    Venus
  7. Flyby

    Carrier bus flies by Venus and relays the descent craft's data

    The flight platform page records that as it flew by Venus the flight platform acted as a data relay for the brief life of the descent module, and then continued on into a heliocentric orbit; it prints no closest-approach distance. Recorded at day precision because the launch/orbital information page's flyby row prints a closest approach time of 1982-03-01 00:00:00, a midnight placeholder rather than an observed time, and a periapsis of 0.00.

    Venus
  8. Mission end

    Last interplanetary data from the flight platform

    The descent craft page records that the lander survived for 127 minutes against a planned design life of 32 minutes, in an environment with a temperature of 457 degrees C and a pressure of 89 Earth atmospheres. The flight platform page records that the engine was fired on 10 June and 14 October 1982 as a test to provide engineering data for the upcoming flyby of Comet Halley by the Vega spacecraft, and that the platform transmitted data from interplanetary space until at least 25 April 1983.

Mission architecture

Vehicles

  • Venera 13 Flight Platform · Spacecraft

    Destinations: Venus

    • Venera 13 Descent Craft · Lander · completed

      Destinations: Venus

Trajectory record

Trajectory dataset not yet available

No verified trajectory dataset is committed for this mission, so Mission Atlas renders no path.

Provenance

Sources

Each source is listed once and labeled with the mission, event, trajectory, or destination/body context it supports.

Data verified through September 3, 2026