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Cosmos-320

Cosmos-320 ( DS-MO No. 2) is a Soviet research satellite of the Cosmos series of spacecraft of the DS-MO type, launched in 1970 for remote sensing of the Earth , the study of the Earth’s atmosphere and the development of an aerodynamic orientation system.

Cosmos-320
" DS-MO " No. 2
CustomerIFZRAN
ManufacturerUnion of Soviet Socialist Republics OKB-586
OperatorUnion of Soviet Socialist Republics USSR Ministry of Defense
TasksRemote sensing , atmospheric research, development of an aerodynamic orientation system
SatelliteSatellite
Launch padUnion of Soviet Socialist Republics Kapustin Yar , Mayak-2 Playground
Carrier rocket63С1 Cosmos-2
LaunchJanuary 16, 1970 11:00:00 UTC
Descent from orbitFebruary 10, 1970
NSSDC ID1970-005A
SCN04301
Specifications
Platform" DS-MO "
Weight321 kg
Dimensions6.5 x 1.2 m [1]
Power suppliesChemical batteries
OrientationTo Earth and speed vector
Active lifeten
Orbit elements
Orbit typeDOE
Eccentricity0,00764
Mood48.5 °
Period of treatment90 minutes
Apocenter342 km
Pericenter240 km
Target equipment
Topaz-25-Mtelevision equipment
Actin-1actinometric equipment [1]
“TFA-3A”, “TFA-3B”telephotometers [1]
RIM-901pressure gauge [1]
RB-21, RV-2PInstruments for measuring solar radiation [1]
Project site

Content

Creation History

In December 1959, the Interdepartmental Scientific and Technical Council for Space Research was created at the USSR Academy of Sciences , headed by Academician M.V. Keldysh , which is charged with developing thematic plans for the creation of spacecraft, issuing key thematic tasks, and coordinating research work and the development of the upper atmosphere and outer space, the preparation of questions of the organization of international cooperation in space research. [2]

The member of the Presidium of the Interdepartmental Scientific and Technical Council for Space Research is approved by MK K. Yangel . In the field of applied tasks of carrying out such work, NII-4 of the USSR Ministry of Defense was entrusted. [2]

In 1962, the spacecraft “ DS-A1 ”, “ DS-P1 ”, “ DS-MT ” and “ DS-MG ” were included in the second-phase launch program of the “ 63C1 ” launch vehicle . [3]

Design Features

The scientific hardware complex of the Cosmos-320 spacecraft included:

  • television equipment "Topaz-25-M" - shooting and transmission of television images to ground stations;
  • actinometric equipment "Actin-1" consisting of:
- tele photometers TF-3A and TF-3B - measuring the angular distribution of the energy brightness of the outgoing short-wave radiation in the visible , near UV and infrared parts of the spectrum;
- SA-2 spectrum analyzer - measuring the long-wave radiation of the Earth in the spectral range of 8-12 microns;
- RB-21 and RV-2P devices - measurement of reflected solar radiation and Earth's own radiation and atmosphere;
- RIM-901 manometer - measurement and analysis of the flow of neutral molecules (on the spacecraft No. 2).

Cosmos-320 spacecraft flight program

Assignment

The scientific tasks of the spacecraft were:

  • study of changes in the radiation balance of the Earth and its atmosphere in the visible , near ultraviolet and infrared regions of the spectrum
  • obtaining images of the Earth’s cloud cover and underlying surface in order to determine the parameters of the atmospheric conditions and cloud cover
  • determination of the temperature of the underlying surface of the Earth
  • determining the height of the upper boundary of the clouds
  • obtaining a map of the distribution of ozone and water vapor in the atmosphere.

An important technological task of the apparatus was to test and analyze the operation of systems and structures of aerodynamic orientation and aerogyroscopic stabilization.

The experimental director was the Institute of Earth Physics (now the O. I. Schmidt Institute of Earth Physics ).

Run

The Cosmos-320 spacecraft was launched on January 16, 1970, with the launch vehicle 63C1 from the launch pad Mayak-2 of the Kapustin Yar Cosmodrome. [four]

Experiment Results

The satellite worked until February 10, 1970 .

As a result of the experiments, a comprehensive program was carried out to study the solar radiation reflected from the Earth in the visible , ultraviolet and infrared parts of the spectrum, as well as the Earth's own radiation in the infrared range.

Methods were developed for determining some parameters of the atmosphere , cloud cover and the earth's surface, which were recommended for practical use in meteorology .

Successfully developed aerodynamic orientation and aerogiroscopic stabilization.

Also, for the first time, reception of telemetric information, in particular, a television image of the Earth transmitted from the satellite by Topaz-25-M equipment, was carried out directly in OKB-586 in a laboratory specially created for these purposes.

See also

  • Cosmos (spacecraft)
  • Dnepropetrovsk satellite

Notes

  1. ↑ 1 2 3 4 5 Rockets and spacecraft of the Design Bureau "Southern", 2001 , p. 116.
  2. ↑ 1 2 Rockets and spacecraft of the Design Bureau "Southern", 2001 , p. 109.
  3. ↑ Rockets and spacecraft of the Design Bureau "Southern", 2001 , p. 110.
  4. ↑ NSSDC Master Catalog Search .

Literature

  • Rockets and spacecraft Design Bureau "Southern" / Under the total. ed. S. N. Konyukhova . - Dnepropetrovsk: LLC “Kolograf”, LLC RA “Tandem-U”, 2001. - T. 1. - 240 p. - 1100 copies. - ISBN 966-7482-00-6 .
  • Zaitsev Yu. I. Satellites "Space" . - M .: Nauka , 1975. - (Problems of science and technological progress). - 38,000 copies.

Articles

  • V. Agapov. By the launch of the first satellite of the DS series // Cosmonautics News: journal. - M .: Videocosmos, 1997.- T. 7 , no. March 10-23 , No. 6/147 . Archived February 2, 2014.
  • Marchenko Marina. Satellites of the Cosmos series // Technology of Youth: Journal. - M. , 1979. - No. 12 . - S. 40-41 .

Links

  • NSSDC Master Catalog Search . NSSDC Master Catalog Search. Date of treatment May 3, 2013. Archived May 23, 2013.
Source - https://ru.wikipedia.org/w/index.php?title=Cosmos-320&oldid=95455262


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