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 Design and development  





2 Specifications (VM-T)  





3 See also  





4 References  





5 External links  














Myasishchev VM-T






Български
Čeština
Deutsch
Español
فارسی
Français
Italiano
Magyar

Português
Русский
Slovenščina
Тоҷикӣ
Українська
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
 


VM-T Atlant
VM-T with the 3GT payload container at the Zhukovsky Air Show in 2005
Role Outsize cargo transport
Manufacturer Myasishchev
Designer Vladimir Mikhailovich Myasishchev
First flight 29 April 1981
Introduction January 1982
Retired 1989
Status Retired
Primary users Soviet Air Force
Russian Federal Space Agency (Soviet space program)
Number built 2
Developed from Myasishchev M-4

The Myasishchev VM-T Atlant (Russian: Мясищев ВМ-Т «Атлант» ("Atlas"), with the "VM-T" ("BM-T") standing for Vladimir Myasishchev – Transport) was a variant of Myasishchev's M-4 Molot bomber (the "3M"), re-purposed as a strategic-airlift airplane. The VM-T was modified to carry rocket boosters and the Soviet space shuttles of the Buran program. It is also known as the 3M-T.

Design and development[edit]

The design was conceived in 1978 when Myasishchev was asked to solve the problem of transporting rockets and other large space vehicles to the Baikonur Cosmodrome. Engineers used an old 3M (a modified M-4 bomber) and replaced the empennage with dihedralled horizontal stabilizers with large, rectangular end-plate tailfins to accommodate payloads measuring as large as twice the diameter of the aircraft's fuselage. A large, aerodynamically optimized cargo container, placed on top of the aircraft, would contain the freight. In addition, a new control system was added to the plane to compensate for the added weight.

The Atlant first flew in 1981 and made its first flight with cargo in January 1982.[1] Its main task was to ferry Energia rocket boosters from their development plant to the Baikonur Cosmodrome. On several occasions, the then-incomplete Soviet space shuttle Buran was piggybacked to the Cosmodrome as well.[1]

Two Atlants were built. They were replaced in 1989 by Antonov's An-225 Mriya. One Atlant (RF-01502) is kept at the Zhukovsky International AirportinRussia owned by TsAGI and Gromov Flight Research Institute, the other one (RA-01402) at Dyagilevo (air base)inRyazan. 0GT was the Buran spaceplane without tailplane and equipment, 1GT was the hydrogen tank of the Energia rocket, 2GT was the engine frame and front aerodynamic cover of Energia and 3GT was the oxygen tank of Energia. All configurations were equipped with aerodynamic cover to decrease the drag.[2]

Specifications (VM-T)[edit]

Data from Jane's aircraft recognition guide 1996,[3] VM-T Atlant's mains characteristics,[4]

General characteristics

  • 0GT payload container 45,300 kg (99,869 lb) - (38.45 m (126 ft) long, 23.8 m (78 ft) Buran wingspan)[5][6]
  • 1GT payload container 31,500 kg (69,446 lb) - (44.46 m (146 ft) long, 7.78 m (26 ft) diameter)[6]
  • 2GT payload container 30,000 kg (66,139 lb) - (26.41 m (87 ft) long, 7.75 m (25 ft) diameter)[6]
  • 3GT payload container 15,000 kg (33,069 lb) - (16.67 m (55 ft) long, 7.75 m (25 ft) diameter)[6]
  • 0GT payload container 126,500 kg (278,885 lb)[6]
  • 1GT payload container 112,700 kg (248,461 lb)[6]
  • 2GT payload container 111,200 kg (245,154 lb)[6]
  • 3GT payload container 96,200 kg (212,085 lb)[6]
  • 0GT payload container 187,000 kg (412,264 lb)[6]
  • 1GT payload container 170,500 kg (375,888 lb)[6]
  • 2GT payload container 169,000 kg (372,581 lb)[6]
  • 3GT payload container 152,200 kg (335,544 lb)[6]
  • 0GT payload container 138,500 kg (305,340 lb)[6]
  • 1GT payload container 129,500 kg (285,499 lb)[6]
  • 2GT payload container 128,000 kg (282,192 lb)[6]
  • 3GT payload container 111,200 kg (245,154 lb)[6]

Performance

See also[edit]

Related development

Aircraft of comparable role, configuration, and era

References[edit]

  • ^ "VM-T Atlant (Bison B mod.) :: Ruslet".
  • ^ Rendall (1996). Jane's aircraft recognition guide. HarperCollinsPublishers. p. 189. ISBN 0-00-470980-2.
  • ^ Petrovitch, Vassili. "VM-T Atlant Caracteristics". www.buran-energia.com. Retrieved 18 October 2019.
  • ^ This equates to a Buran with tail fairing
  • ^ a b c d e f g h i j k l m n o p q Gordon, Yefim (2003). Myasishchev M-4 and 3M. Hinkley: Midland. pp. 93–108. ISBN 978-1-85780-152-1.

  • External links[edit]


    Retrieved from "https://en.wikipedia.org/w/index.php?title=Myasishchev_VM-T&oldid=1131165989"

    Categories: 
    Myasishchev aircraft
    1980s Soviet cargo aircraft
    Quadjets
    Aircraft first flown in 1981
    Aircraft related to spaceflight
    Hidden categories: 
    Articles with short description
    Short description matches Wikidata
    Short description is different from Wikidata
    Aircraft specs templates using more performance parameter
    Commons category link is on Wikidata
     



    This page was last edited on 2 January 2023, at 21:49 (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