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Mission record

Venera 11

Also known as Venera 11 Flight Platform, Venera11

Soviet Academy of Sciences · Launched

Explore trajectory

Completed · Partial success

One of a pair of identical Soviet spacecraft built for the September 1978 Venus launch window, each comprising a descent craft mounted on a flyby bus rather than the orbiter used on earlier missions. The flight platform carried instruments to study solar-wind composition, gamma-ray bursts, ultraviolet radiation and the electron density of the ionosphere of Venus; the descent craft studied the detailed chemical composition of the atmosphere, the nature of the clouds, the thermal balance of the atmosphere and the composition and mechanical properties of the surface. The descent craft made a soft landing and transmitted to the flight platform for 95 minutes after touchdown, but the lens cover on the imaging system failed to eject so no images were returned, and the soil sample was not placed correctly into the chamber so the planned analysis could not be done.

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 and the descent craft page both print the launch time as 03:25:39 UT on 1978-09-09. The flight platform page names the booster in its own text as a Proton-K while all three pages print Proton Booster Plus Upper Stage and Escape Stages under Launch Vehicle. THE TWO ENUMERATION SPINES DISAGREE ON WHAT THIS SPACECRAFT WAS: NSSDCA's general chronology classifies it Venus Orbiter and Lander while its Venus-specific chronology classifies the same flight Venus Flyby Bus and Lander. The descent craft page settles it in NSSDCA's own words - the descent craft was mounted on a flyby bus, not an orbiter as on earlier missions - and this record follows the pages rather than the chronology row.

    Earth
  2. Deployment

    Descent craft separates from the flight platform

    The descent craft page records that the descent module separated from its flight platform on December 23, 1978, and entered the nightside Venus atmosphere two days later at 11.2 km/sec.

    Venus
  3. Flyby

    Flight platform passes Venus at approximately 34,000 km altitude

    The flight platform page records the encounter with Venus on December 25, 1978 at approximately 34,000 km altitude, and that it acted as a data relay for the descent craft for 95 minutes. Recorded at day precision because the page hedges the altitude with the word approximately and its launch/orbital information page prints a closest approach time of 1978-12-25 00:00:00, a midnight placeholder rather than an observed time. That page's own 6.62 RV, against its stated 1 RV = 6052 km, is about 40,000 km rather than the 34,000 km the master catalog prints, and the disagreement is recorded rather than resolved. READ AS THE PERIAPSIS BY INFERENCE, NOT BY READING: the committed excerpt flattens that table to five headers followed by three values, Periapsis Apoapsis Period Inclination Eccentricity 6.62 RV 0.000 degrees 0.00000, so which column 6.62 RV sits in cannot be read off the excerpt and is taken from its position as the first value.

    Venus
  4. Landing

    Soft landing at 14 S, 299 E

    The descent craft page records a soft landing on the surface at 03:24 UT on 25 December after a descent time of approximately 1 hour, with a touchdown speed of 7-8 m/s at 14 S, 299 E. That sentence prints no year, and the year comes from the descent craft's own launch/orbital information page, which prints a Lander row with an epoch start of 1978-12-25 03:24:00 and a Decay Date of 1978-12-25 - a single page printing a complete date and time, not a time taken from one sentence and a date from another.

    Venus
  5. Loss of contact

    Final contact with the flight platform

    The flight platform page records that final contact with Venera 11 was on 1 February 1980, after a trajectory maneuver on 7 February 1979 used up most of its propellant and left it in a 1.116 x 1.715 AU orbit.

  6. Milestone

    Two mid-course corrections en route to Venus

    Both pages record two mid-course corrections, on 16 September and 17 December. Carried without a timestamp because the sentences that print those days print no year.

Mission architecture

Vehicles

  • Venera 11 Flight Platform · Spacecraft

    Destinations: Venus

    • Venera 11 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