Kosmos 163

In the following article we will explore the impact that Kosmos 163 has had on different aspects of today's society. From its origin to its relevance today, Kosmos 163 has been a topic of interest for researchers, experts and the general public. Throughout this article, we will analyze the different perspectives related to Kosmos 163, as well as the implications it has had in areas such as technology, culture, politics and economics. Additionally, we will examine how Kosmos 163 has influenced and changed the way we interact, communicate and navigate in today's world. Without a doubt, Kosmos 163 has left a significant mark on our society and will continue to be a relevant topic for the future.

Kosmos 163
Mission typeMicrometeoroid research
COSPAR ID1967-056A Edit this at Wikidata
SATCAT no.02832
Mission duration128 days
Spacecraft properties
Spacecraft typeDS-U2-MP
ManufacturerYuzhnoye
Launch mass357 kg[1]
Start of mission
Launch date5 June 1967, 05:03:00 GMT
RocketKosmos-2I 63SM
Launch siteKapustin Yar, Site 86/1
ContractorYuzhnoye
End of mission
Decay date11 October 1967
Orbital parameters
Reference systemGeocentric[2]
RegimeLow Earth
Perigee altitude244 km
Apogee altitude611 km
Inclination48.4°
Period93.1 minutes
Epoch5 June 1967

Kosmos 163 (Russian: Космос 163 meaning Cosmos 163), also known as DS-U2-MP No.2, was a Soviet satellite which was launched in 1967 as part of the Dnepropetrovsk Sputnik programme. It was a 357 kilograms (787 lb) spacecraft, which was built by the Yuzhnoye Design Office, and was used to investigate micrometeoroids and cosmic dust particles in near-Earth space.[3]

A Kosmos-2I 63SM carrier rocket was used to launch Kosmos 163 into low Earth orbit. The launch took place from Site 86/1 at Kapustin Yar.[4] The launch occurred at 05:03:00 GMT on 5 June 1967, and resulted in the successful insertion of the satellite into orbit.[5] Upon reaching orbit, the satellite was assigned its Kosmos designation, and received the International Designator 1967-056A.[1] The North American Air Defense Command assigned it the catalogue number 02832.[1]

Kosmos 163 was the second of two DS-U2-MP satellites to be launched, after Kosmos 135.[5][6] It was operated in an orbit with a perigee of 244 kilometres (152 mi), an apogee of 611 kilometres (380 mi), an inclination of 48.4°, and an orbital period of 93.1 minutes.[2] It decayed from its orbit and reentered the atmosphere on 11 October 1967.[7]

See also

References

  1. ^ a b c "Cosmos 163: Display 1967-056A". nssdc.gsfc.nasa.gov. NASA. 27 February 2020. Retrieved 17 April 2020. Public Domain This article incorporates text from this source, which is in the public domain.
  2. ^ a b "Cosmos 163: Trajectory 1967-056A". nssdc.gsfc.nasa.gov. NASA. 27 February 2020. Retrieved 17 April 2020. Public Domain This article incorporates text from this source, which is in the public domain.
  3. ^ Wade, Mark. "DS-U2-MP". Encyclopedia Astronautica. Archived from the original on 5 January 2009. Retrieved 23 December 2009.
  4. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 23 December 2009.
  5. ^ a b Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Archived from the original on 18 June 2012. Retrieved 23 December 2009.
  6. ^ Krebs, Gunter. "DS-U2-MP". Gunter's Space Page. Retrieved 23 December 2009.
  7. ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 23 December 2009.


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