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Mars 5

NSSDCA/COSPAR ID: 1973-049A

Description

Mars 4, 5, 6, and 7 comprised an associated group of Soviet spacecraft launched towards Mars in July and August of 1973. The Mars 5 automatic station was designed to orbit Mars and return information on the composition, structure, and properties of the martian atmosphere and surface. The spacecraft was also designed to act as a communications link to the Mars 6 and 7 landers. The orbiter operated only a few days and returned atmospheric data and images of a small portion of the martian southern hemisphere.

Mission Profile

Mars 5 was launched into Earth orbit by a Proton SL-12/D-1-e booster, and propelled from its orbital platform into a Mars transfer trajectory at 20:15 UT on 25 July 1973. The fully fueled launch mass of the orbiter was 3440 kg. After a mid-course correction burn on 3 August, the spacecraft reached Mars on 12 February 1974 at 15:45 UT and was inserted into an elliptical 1755 km x 32,555 km, 24 hr, 53 min. orbit with an inclination of 35.3 degrees. Mars 5 collected data for 22 orbits until a loss of pressurization in the transmitter housing ended the mission. About 60 images were returned over a nine day period showing swaths of the area south of Valles Marineris, from 5 N, 330 W to 20 S, 130 W. Measurements by other instruments were made near periapsis along 7 adjacent arcs in this same region.

Scientific Instrumentation

Mars 5 was equipped with a television imaging system consisting of two cameras. One, called Vega, was f/2.8 with a focal length of 52 mm, a 23 x 22.5 mm frame, and a 35.7 degree look angle. The other camera, Zufar, was f/4.5 with a 350 mm focal length, 23 x 22.5 mm frame, and a 5.67 degree look angle. The images were taken through blue, red, and green filters in addition to a special orange filter and could be facsimile scanned at 1000 x 1000 or 2000 x 2000 pixels and transmitted to Earth. The cameras provided pictures with resolutions of 100 m to 1 km. In addition, there was a single-line scanning device with a 30 degree field of view to provide panoramic images in the visible and near-infrared.

The spacecraft was also equipped with a Lyman-Alpha photometer to search for hydrogen in the upper atmosphere, a magnetometer, plasma ion traps and a narrow angle electrostatic plasma sensor to stidy the solar wind, an infrared radiometer (8-40 microns) to measure surface temperature, a radio telescope polarimeter (3.5 cm) to probe the subsurface dielectric constant, two polarimeters (0.32-0.70 microns) to characterize surface texture, and a spectrometer (0.3 - 0.8 microns) to study emissions in the upper atmosphere.

There were four photometers on board: one for 2 carbon dioxide bands to obtain altitude profiles, one at 0.35 - 0.7 microns for albedo and color studies, one in the water vapor band (1.38 microns) to study water in the atmosphere, and a UV photometer (0.26 and 0.28 microns) to measure ozone. The probe was equipped with a radio-occultation experiment to profile atmospheric density and a dual-frequency radio occultation experiment to profile ionospheric density. The spacecraft also carried French experiments, one called Zhemo to study the distribution and intensity of fluxes of solar protons and electrons and one known as Stereo-2 to study solar radio emissions.

Scientific Results

Data returned from orbit by the Mars 5 infrared radiometer showed a maximum surface temperature of 272 K, 230 K near the terminator and 200 K at night. Thermal inertia of soil was consistent with grain sizes of 0.1 to 0.5 mm, polarization data showed grain sizes smaller than 0.04 mm in aeolian deposits. Six altitude profiles were measured by the CO2 photometer. U, Th, and K composition similar to terrestrial mafic rocks were found. A dielectric constant from 2.5 to 4 was measured at depths of several tens of cm. A high water vapor content (100 precipitable microns) was found south of Tharsis region. An ozone layer was detected at 40 km altitude with about one-thousandth the concentration of Earth's. The exosphere temperature was measured at 295-355 K, 10 K lower temperatures were found from 200 to 87 km. A small magnetic field was postulated, about .0003 Earth's. Mars 5 also performed a radio occultation experiment and the results, in concert with results from Mars 4 and 6 occultation measurements, showed the existence of a nightside ionosphere with a maximum electron density of 4600 per cubic cm at an altitude of 110 km and a near surface atmospheric pressure of 6.7 mbar.

Spacecraft image for illustrative purposes - not necessarily in the public domain.

Alternate Names

  • M-73 No.53S
  • 06754

Facts in Brief

Launch Date: 1973-07-25
Launch Vehicle: Proton Booster Plus Upper Stage and Escape Stages
Launch Site: Tyuratam (Baikonur Cosmodrome), U.S.S.R
Mass: 2270.0 kg

Funding Agency

  • Unknown (U.S.S.R)

Disciplines

  • Planetary Science
  • Space Physics

Additional Information

Questions or comments about this spacecraft can be directed to: Dr. David R. Williams.

 

Personnel

NameRoleOriginal AffiliationE-mail
Mr. Artem IvankovGeneral ContactLavochkin Associationartem.ivankov@laspace.ru

Selected References

Shelton, W., Soviet space exploration - the first decade, Arthur Barker Ltd., Unnumbered, London, England, 1969.

Moroz, V. I., Preliminary results of studies conducted on the Soviet automatic stations Mars 4, Mars 5, Mars 6, and Mars 7, Cosmic Res., 13, No. 1, 1-6, July 1975.

Harvey, B., The new Russian space programme from competition to collaboration, John Wiley & Sons, Chichester, England, 1996.

Perminov, V. G., The difficult road to Mars - A brief history of Mars exploration in the Soviet Union, NASA, No. 15, Wash, DC, July 1999.

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