Image of Viking Lander
Viking 2 Lander Mission Profile

Following launch and a 333 day cruise to Mars, the Viking 2 Orbiter began returning global images of Mars prior to orbit insertion. The orbiter was inserted into a 1500 x 33,000 km, 24.6 hr Mars orbit on 7 August 1976 and trimmed to a 27.3 hr site certification orbit with a periapsis of 1499 km and an inclination of 55.2 degrees on 9 August. Imaging of candidate sites was begun and the landing site was selected based on these pictures and the images returned by the Viking 1 Orbiter. The lander and its aeroshell separated from the orbiter on 3 September 19:39:59 UT. At the time of separation, the lander was orbiting at about 4 km/s. After separation rockets fired to begin lander deorbit. After a few hours, at about 300 km altitude, the lander was reoriented for entry. The aeroshell with its ablatable heat shield slowed the craft as it plunged through the atmosphere. During this time, entry science experiments were performed. At 6 km altitude at about 250 m/s the 16 m diameter lander parachutes were deployed. Seven seconds later the aeroshell was jettisoned, and 8 seconds after that the three lander legs were extended. In 45 seconds the parachute had slowed the lander to 60 m/s. At 1.5 km altitude, retro-rockets were ignited and fired until landing 40 seconds later at about 2.4 m/s. The landing rockets used an 18 nozzle design to spread the hydrogen and nitrogen exhaust over a wide area. It was determined that this would limit surface heating to no more than 1 degree C and that no more than 1 mm of the surface material would be stripped away.

The Viking 2 Lander touched down about 200 km west of the crater Mie in Utopia Planitia at 48.269 deg N latitude and 225.990 deg W longitude at a reference altitude of 4.23 km relative to a reference ellipsoid with an equatorial radius of 3397.2 km and a flatness of 0.0105 (47.967 deg N, 225.737 deg W planetographic) at 22:58:20 UT (9:49:05 a.m. local Mars time). Approximately 22 kg of propellants were left at landing. Due to radar misidentification of a rock or highly reflective surface, the thrusters fired an extra time 0.4 seconds before landing, cracking the surface and raising dust. The lander settled down with one leg on a rock, tilted at 8.2 degrees. The cameras began taking images immediately after landing. The Viking 2 Lander operated on the surface for 1281 Mars days and was turned off on April 11, 1980 when its batteries failed.

For a detailed description of the Viking mission and experiments, see "Scientific Results of the Viking Project," J. Geophys. Res., v. 82, n. 28, 1977.

Source: Viking Project Information - NSSDC


  1. Masursky, H., and Crabill, N. L., Viking landing sites: Selection and certification, Science, 193, 809-812, Aug. 1976.
  2. Soffen, G. A., Scientific results of the Viking mission, Science, 194, No. 4271, 1274-1276, Dec. 1976.
  3. Soffen, G. A., The Viking project, J. Geophys. Res., 82, No. 28, 3959-3970, Sep. 1977.
  4. Masursky, H., and Crabill, N. L., Viking landing sites: Selection and certification, Science, 193, 809-812, Aug. 1976.
  5. Soffen, G. A., and Snyder, C. W., First Viking mission to Mars, Science, 193, 759-766, Aug. 1976.
  6. Tyler, G. L., Campbell, D. B., Downs, G. S., Green, R. R., and Moore, H. J., Radar characteristics of Viking 1 landing sites, Science, 193, 812-815, Aug. 1976.

Objectives Lander Orbiter Lander 1 Orbiter 1
Lander 2 Orbiter 2 Images Links
Viking Home Page Spacecraft Home Page


Wednesday, 31-Dec-1969 18:00:00 CST