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 Mission  





2 Parameters  





3 References  





4 External links  














Kosmos 379






Български
Magyar
Македонски

Polski
Português
Русский
Српски / srpski
Srpskohrvatski / српскохрватски
Українська

 

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
 
















Appearance
   

 






From Wikipedia, the free encyclopedia
 


Kosmos 379
LK lander
Mission typeSpacecraft test
OperatorSoviet space program
COSPAR ID1970-099A Edit this at Wikidata
SATCAT no.4760
Mission duration12 years, 9 months and 28 days (in orbit)
Spacecraft properties
Spacecraft typeT2K No.1
ManufacturerOKB-1
Launch mass7,495 kilograms (16,524 lb)
Start of mission
Launch date24 November 1970, 11:00:00 (1970-11-24UTC11Z) UTC
RocketSoyuz-L
Launch siteBaikonur 31/6
End of mission
Decay date21 September 1983
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Eccentricity0.004161
Perigee altitude198 kilometres (123 mi)
Apogee altitude253 kilometres (157 mi)
Inclination51.6 degrees
Period88.7 min
T2K No.2 →
 

Kosmos 379 (Russian: Космос 379 meaning "Cosmos 379"), also known as T2K No.1, was an unmanned test of the LK (the Soviet counterpart of the Apollo Lunar Module) in Earth orbit.

Mission[edit]

Earth orbit simulated propulsion system operations of a nominal lunar landing mission. Kosmos 379 entered a 192 to 232 km low Earth orbit. After three days it fired its motor to simulate hover and touchdown on the moon, in imitation of a descent to the lunar surface after separation of the Blok D lunar crasher propulsion module. The engine firing changed its orbit from 192 km X 233 km to 196 km X 1206 km (delta-V = 263 m/s).

After a simulated stay on the Moon, it increased its speed by 1.518 km/s, simulating ascent to lunar orbit making the final apogee 14,035 km. These main maneuvers were followed by a series of small adjustments simulating rendezvous and docking with the Soyuz 7K-L3. The LK lander tested out without major problems and decayed from orbit on September 21, 1983.[1]

Parameters[edit]

References[edit]

  1. ^ Mark Wade. "Soyuz 11A511L". Encyclopedia Astronautica. Retrieved 27 December 2016.

External links[edit]

  • t
  • e

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=Kosmos_379&oldid=1226329443"

    Categories: 
    Kosmos satellites
    Soviet lunar program
    1970 in the Soviet Union
    Spacecraft launched in 1970
    Soviet Union spacecraft stubs
    Hidden categories: 
    Articles with short description
    Short description is different from Wikidata
    Articles containing Russian-language text
    All stub articles
     



    This page was last edited on 29 May 2024, at 23:20 (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