To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

From Wikipedia, the free encyclopedia

Kosmos 29
Mission typeOptical imaging reconnaissance
OperatorOKB-1
COSPAR ID1964-021A
SATCAT no.00791
Mission duration8 days
Spacecraft properties
Spacecraft typeZenit-2
ManufacturerOKB-1
Launch mass4780 kg [1]
Start of mission
Launch date25 April 1964, 10:19:00 GMT
RocketVostok-2 s/n R15001-01
Launch siteBaikonur, Site 31/6
ContractorOKB-1
End of mission
DisposalRecovered
Landing date3 May 1964
Orbital parameters
Reference systemGeocentric [2]
RegimeLow Earth
Perigee altitude203 km
Apogee altitude296 km
Inclination65.1°
Period89.5 minutes
Epoch25 April 1964
 

Kosmos 29 (Russian: Космос 29 meaning Cosmos 29) or Zenit-2 No.19 was a Soviet, a first generation, low resolution, optical film-return reconnaissance satellite which was launched in 1964. A Zenit-2 spacecraft, Kosmos 29 was the seventeenth of eighty-one such satellites to be launched[3] and had a mass of 4,780 kilograms (10,540 lb).

A Vostok-2 rocket, serial number R15001-01,[4] was used to launch Kosmos 29. The launch took place at 10:19 GMT on 25 April 1964, using Site 31/6 at the Baikonur Cosmodrome.[5] Following its successful arrival in orbit the spacecraft received its Kosmos designation, along with the International Designator 1964-021A and the Satellite Catalog Number 00791.[6]

Kosmos 29 was operated in a low Earth orbit. On 25 April 1964, it had a perigee of 203 kilometres (126 mi), an apogee of 296 kilometres (184 mi), with inclination of 65.1° and an orbital period of 89.5 minutes. After eight days in orbit, the satellite was deorbited on 3 May 1964 with its return capsule descending by parachute for recovery by Soviet forces.[7][8]

YouTube Encyclopedic

  • 1/5
    Views:
    51 701 363
    2 725
    66 679
    18 020
    1 689
  • NASA Live - Earth From Space (HDVR) ♥ ISS LIVE FEED #AstronomyDay2017 | Subscribe now!
  • Tallest Mountains in the Solar System
  • Oort Cloud Myth Continues to Crumble | Space News
  • Armageddon' asteroid BENNU:Nasa to launch Osiris-Rex probe to Investigate
  • [Proton] Launch of GLONASS M17, M18 & M19 Spacecraft

Transcription

References

  1. ^ https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1964-021A - 27 February 2020
  2. ^ https://nssdc.gsfc.nasa.gov/nmc/spacecraft/displayTrajectory.action?id=1964-021A - 27 February 2020
  3. ^ Krebs, Gunter. "Zenit-2 (11F61)". Gunter's Space Page. Archived from the original on 31 December 2011. Retrieved 15 December 2013.
  4. ^ Wade, Mark. "Vostok 8A92". Encyclopedia Astronautica. Archived from the original on 22 August 2016. Retrieved 13 December 2013.
  5. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 15 December 2013.
  6. ^ "Cosmos 29". National Space Science Data Center. Retrieved 15 December 2013.
  7. ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 15 December 2013.
  8. ^ Wade, Mark. "Zenit-2". Encyclopedia Astronautica. Archived from the original on 21 April 2012. Retrieved 15 December 2013.
This page was last edited on 28 January 2021, at 18:45
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.