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1 See also  





2 References  














Kosmos 196






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From Wikipedia, the free encyclopedia
 


This is an old revision of this page, as edited by WDGraham (talk | contribs)at14:07, 16 December 2013 (References: recategorise, genfixes, replaced: Category:1967 in spaceflight  Category:Spacecraft launched in 1967 using AWB). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.
(diff)  Previous revision | Latest revision (diff) | Newer revision  (diff)

Kosmos 196
Mission typeSolar research
COSPAR ID1967-125A Edit this at Wikidata
SATCAT no.03074Edit this on Wikidata
Spacecraft properties
Spacecraft typeDS-U1-G
ManufacturerYuzhnoye
Launch mass291 kilograms (642 lb)[1]
Start of mission
Launch date19 December 1967, 06:30:07 (1967-12-19UTC06:30:07Z) UTC
RocketKosmos-2I 63S1
Launch siteKapustin Yar 86/1
End of mission
Decay date7 July 1968 (1968-07-08)
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Perigee altitude220 kilometres (140 mi)
Apogee altitude810 kilometres (500 mi)
Inclination48.8 degrees
Period94.9 minutes
 

Kosmos 196 (Russian: Космос 196 meaning Cosmos 196), also known as DS-U1-G No.2, was a Soviet satellite which was launched in 1967 as part of the Dnepropetrovsk Sputnik programme. It was a 291-kilogram (642 lb) spacecraft,[1] which was built by the Yuzhnoye Design Bureau, and was used to study the effects of solar activity on the upper atmosphere.[2]

AKosmos-2I 63S1 carrier rocket was used to launch Kosmos 196 into low Earth orbit. The launch took place from Site 86/1atKapustin Yar.[3] The launch occurred at 06:30:07 UTC on 19 December 1967, and resulted in the successfully insertion of the satellite into low Earth orbit.[4] Upon reaching orbit, the satellite was assigned its Kosmos designation, and received the International Designator 1967-125A.[5] The North American Aerospace Defense Command assigned it the catalogue number 03074.

Kosmos 196 was the second of two DS-U1-G satellites to be launched,[2] after Kosmos 108.[6] It was operated in an orbit with a perigee of 220 kilometres (140 mi), an apogee of 810 kilometres (500 mi), 48.8 degrees of inclination, and an orbital period of 94.9 minutes.[7] It completed operations on 7 February 1968.[1] On 7 July 1968, it decayed from orbit and reentered the atmosphere.[7]

See also

References

  1. ^ a b c "World Civil Satellites 1957-2006". Space Security Index. Retrieved 2009-11-14.
  • ^ a b Wade, Mark. "DS-U1-G". Encyclopedia Astronautica. Retrieved 2009-11-14.
  • ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 2009-11-14.
  • ^ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Retrieved 2009-11-14.
  • ^ "Cosmos 196". NSSDC Master Catalog. US National Space Science Data Center. Retrieved 2009-11-14.
  • ^ Krebs, Gunter. "DS-U1-G". Gunter's Space Page. Retrieved 2009-11-14. [dead link]
  • ^ a b McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 2009-11-14.

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  • Retrieved from "https://en.wikipedia.org/w/index.php?title=Kosmos_196&oldid=586338593"

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    This page was last edited on 16 December 2013, at 14:07 (UTC).

    This version of the page has been revised. Besides normal editing, the reason for revision may have been that this version contains factual inaccuracies, vandalism, or material not compatible with the Creative Commons Attribution-ShareAlike License.



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