Jump to content
 







Main menu
   


Navigation  



Main page
Contents
Current events
Random article
About Wikipedia
Contact us
Donate
 




Contribute  



Help
Learn to edit
Community portal
Recent changes
Upload file
 








Search  

































Create account

Log in
 









Create account
 Log in
 




Pages for logged out editors learn more  



Contributions
Talk
 



















Contents

   



(Top)
 


1 Orbiter  





2 Lander  





3 See also  





4 References  














Venera 10






Afrikaans
العربية

Български
Català
Čeština
Español
Euskara
فارسی
Français
Հայերեն
Hrvatski
Ido
Bahasa Indonesia
עברית
Magyar
Nederlands

Norsk bokmål
Occitan
Polski
Português
Русский
Slovenčina
Српски / srpski
Suomi
Svenska
Tiếng Vit

 

Edit links
 









Article
Talk
 

















Read
Edit
View history
 








Tools
   


Actions  



Read
Edit
View history
 




General  



What links here
Related changes
Upload file
Special pages
Permanent link
Page information
Cite this page
Get shortened URL
Download QR code
Wikidata item
 




Print/export  



Download as PDF
Printable version
 




In other projects  



Wikimedia Commons
 
















Appearance
   

 






From Wikipedia, the free encyclopedia
 


Venera 10
Venera 10
Mission typeVenus orbiter / lander
OperatorLavochkin
COSPAR ID
  • 1975-054D (lander)
  • SATCAT no.
  • 8423[2]
  • Mission durationTravel: 4 months and 9 days
    Orbiter: 144 days
    Lander: 65 minutes
    Last contact: 286 days
    Spacecraft properties
    Spacecraft type4V-1 No. 661[3]
    ManufacturerLavochkin[3]
    Launch mass5,033 kg (11,096 lb)[3]
    BOL mass2,230 kg (4,920 lb)
    Landing mass1,560 kg (3,440 lb)
    Dimensions2.7 m × 2.3 m × 5.7 m (8.9 ft × 7.5 ft × 18.7 ft)
    Start of mission
    Launch dateJune 14, 1975 (1975-06-14), 03:00:31 UTC[3]
    RocketProton with upper and escape stages
    Launch siteBaikonur 81/24[3]
    End of mission
    Last contact"[Orbiter transmitted] data until at least June 1976."[3]
    Orbital parameters
    Reference systemCytherocentric
    Eccentricity0.8798
    Pericytherion altitude1,620 kilometers (1,010 mi)
    Apocytherion altitude113,900 kilometers (70,800 mi)
    Inclination29.5°
    Period49.4 hours
    Revolution no.71
    Venus orbiter
    Orbital insertionOctober 23, 1975
    Venus lander
    Spacecraft componentVenera 10 descent craft
    Landing date02:17, October 25, 1975
    Landing site15°25′N 291°31′E / 15.42°N 291.51°E / 15.42; 291.51
    (near Beta Regio)
    ← Venera 9
    Venera 11 →
     

    Venera 10 (Russian: Венера-10 meaning Venus 10), or 4V-1 No. 661,[4] was a Soviet uncrewed space missiontoVenus. It consisted of an orbiter and a lander. It was launched on June 14, 1975, 03:00:31 UTC and had a mass of 5033 kg (11096 lb).[5]

    Orbiter[edit]

    When the mission launched, the Soviet Union only disclosed that the mission's objective was to explore Venus and the surrounding space. Western sources speculated that the spacecraft contained a lander.[6]

    The orbiter entered Venus orbit on October 23, 1975. Its mission was to serve as a communications relay for the lander and to explore cloud layers and atmospheric parameters with several instruments and experiments:[7]

    The orbiter consisted of a cylinder with two solar panel wings and a high gain parabolic antenna attached to the curved surface. A bell-shaped unit holding propulsion systems was attached to the bottom of the cylinder, and mounted on top was a 2.4 metres (7 ft 10 in) sphere which held the landers. To reach Venus, the spacecraft traveled in a heliocentric orbit from Earth to the planet with perihelion of 0.72 AU, apohelion of 1.02 AU, eccentricity of 0.17, inclination of 2.3 degrees and orbital period of 294 days.

    Lander[edit]

    On October 23, 1975, the lander separated from the orbiter, and touched down with the sun near zenith, at 05:17 UT, on October 25. A system of circulating fluid was used to distribute the heat load. This system, plus precooling prior to entry, permitted operation of the spacecraft for 65 minutes after landing. During descent, heat dissipation and deceleration were accomplished sequentially by protective hemispheric shells, three parachutes, a disk-shaped drag brake, and a compressible, metal, doughnut-shaped, landing cushion.[7]

    It landed near the border area between Beta Regio and Hyndla Regio[8] (within a 150 km radius of 15°25′N 291°31′E / 15.42°N 291.51°E / 15.42; 291.51), three days after the touchdown of, and 2200 km from Venera 9.[9] Venera 10 measured a surface windspeed of 3.5 m/s. Other measurements included atmospheric pressure at various heights, and temperature, and surface light levels. Venera 10 was the second probe to send back black and white television pictures from the Venusian surface (after Venera 9). Venera 10 photographs showed lava rocks of pancake shape with lava or other weathered rocks in between. Planned 360 degree panoramic pictures could not be taken because, as with Venera 9, one of two camera lens covers failed to come off, limiting pictures to 180 degrees.

    The lander communicated with Earth using the Venera 10 orbiter as a communication relay.[10]

    Lander payload:[7]

    See also[edit]

    References[edit]

    1. ^ "Venera 10 Bus". N2YO.com. Retrieved November 6, 2019.
  • ^ "Venera 10 Descent Craft". N2YO.com. Retrieved November 6, 2019.
  • ^ a b c d e f Siddiqi, Asif A. (2018). Beyond Earth: A Chronicle of Deep Space Exploration, 1958–2016 (PDF). The NASA history series (second ed.). Washington, DC: NASA History Program Office. pp. 128–129. ISBN 978-1-62683-042-4. LCCN 2017059404. SP2018-4041.
  • ^ Zak, Anatoly. "Venera-9 and 10". Russianspaceweb.com. Retrieved April 14, 2013.
  • ^ "Venera 10". National Space Science Data Center. Retrieved April 13, 2013.
  • ^ "Soviet Launches a 2D Spacecraft". The New York Times. Associated Press. June 15, 1975. p. 23.
  • ^ a b c Mitchell, Don P. "First Pictures of the Surface of Venus". Retrieved April 13, 2013.
  • ^ LePage, Andrew (October 22, 2015). "Venera 9 and 10 to Venus". Retrieved February 19, 2016.
  • ^ Interplanetary Spacecraft
  • ^ "Venera 10 Descent Craft". National Space Science Data Center. Retrieved February 25, 2021.

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=Venera_10&oldid=1185748131"

    Categories: 
    Guinevere Planitia quadrangle
    Venera program
    1975 in spaceflight
    1975 in the Soviet Union
    Derelict landers (spacecraft)
    Spacecraft launched in 1975
    Non Earth orbiting satellites of the Soviet Union
    4MV
    Hidden categories: 
    Articles with short description
    Short description matches Wikidata
    Use mdy dates from March 2020
    Pages using gadget WikiMiniAtlas
    Articles containing Russian-language text
     



    This page was last edited on 18 November 2023, at 19:39 (UTC).

    Text is available under the Creative Commons Attribution-ShareAlike License 4.0; additional terms may apply. By using this site, you agree to the Terms of Use and Privacy Policy. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc., a non-profit organization.



    Privacy policy

    About Wikipedia

    Disclaimers

    Contact Wikipedia

    Code of Conduct

    Developers

    Statistics

    Cookie statement

    Mobile view



    Wikimedia Foundation
    Powered by MediaWiki