Mir Core Module

DOS-7
Model of DOS-7 in an early configuration, docked with Kvant-1.
Module statistics
Part ofMir
Launch dateFebruary 20, 1986 (UTC)
ReentryMarch 23, 2001 (UTC)
Mass20,400 kg (45,000 lb)
Length13.13 m (43.1 ft)
Diameter4.5 m (15 ft)
Pressurised volume90 m3 (3,200 cu ft)
Configuration

Diagram of DOS-7 in its original configuration.
DOS-7 seen from Space Shuttle Atlantis during STS-71 in 1995.

The Mir Core Module, also known as the Base Block or DOS-7, was a module of the Mir space station. It was the first module to be launched and operated in low Earth orbit from 1986 until its de-orbiting in 2001. The module was launched on a Proton-K rocket[1] on February 20th, 1986.[2]

A spare of this module, originally designed for Mir-2, later became the Zvezda module used on the International Space Station.

Design

The Mir Core Module was based on the design of its predecessors from the Salyut programme, however, unlike the others, was designed as a habitation module, and thus housed less scientific equipment. Most importantly, it possessed a multi-port docking node on the forward end of the module. This experimental and revolutionary upgrade allowed the station to house an additional five modules, allowing for greater expansion of the station capabilities. The multi-port docking node also had fixtures for the Lyappa arm, which allowed for modules to move themselves around the station. Other changes included larger solar arrays twice the size of Salyut 7's, made out of gallium arsenide (rather than silicon, as was used on Salyut 7's arrays) which saw a 30% improvement in power generation, greater automation and a new docking system, Kurs, in addition to the older Igla system. The station, like its predecessors, had an aft docking node intended for Progress and Soyuz dockings. It also retained its small airlock for science or rubbish disposal.[3]: 105 

Additionally, certain features which were on prior Salyut stations were removed, such as the large imaging camera which had partially obstructed living area on previous stations was removed, allowing for a more comfortable living area.[3]

The interior of the module featured a two-toned appearance (designed by Galina Balashova, who had previously designed interior decor for the Soyuz spacecraft and Salyut stations[4]) as well as fluorescent lighting, one lavatory, two sleeping cabins, exercise equipment, medical equipment and a command centre with television screens for communicating with the RKA Mission Control Center, as well as a new main on-board computer, being the Argon 16B.[3]: 105–106 

The station also had two liquid fuel orbital-maneuvering engines located aft, capable of 300kg of thrust, though became inoperable when Kvant-1 arrived to the station. [3]: 105–106 

History

The Mir Core Module was launched uncrewed on February 20th, 1986[2] and was first docked to and crewed by Soyuz T-15 which later visited Salyut 7 after their stay on Mir, then later returned back to Mir.[5]

Inside the multiple docking node

On April 9th, 1987, Kvant-1 soft-docked with the Mir Core Module, but due to an issue could not achieve a hard-dock until April 11th. Kvant-1 delivered an additional solar array which was mounted to the top of the Mir Core Module later in June.[3]: 111  It was the only module not designed with a propulsion system, nor a Lyappa arm as it was not originally planned to dock with the station.[3]: 162 

Between the years of 1989 and 1996, the modules Kvant-2, Kristall, Spektr and Priroda docked with the Mir Core Module, and each utilised their Lyappa arm to move themselves to their respective docking ports. Kristall was originally positioned opposite of the Kvant-2 module (at the -Y node),[3]: 124  though re-positioned itself between the -X node and -Z node before finally remaining at the -Z node.[6]: 13, 17, 24 

In 1989, the Kvant-2 module delivered a new on-board computer, being the Salyut 5B, which was an improvement over the Argon 16B computer which was already installed.[3]: 41 

In January 1991, Strela, a robotic crane, was installed onto the Mir Core Module by using supports that originally held the launch fairing, which was to assist moving one of Kristall's solar arrays onto Kvant-1.[3]: 128  In 1996, another Strela crane was installed opposite to the existing one.[6]: 38 

During its lifetime, it was proposed at some point for the Buran to replace the Mir Core Module with a new one, and then return the old one back to earth in its payload bay. However, due to complications such as the dissolution of the Soviet Union and the subsequent funding issues that followed with the Buran programme, this never occurred.[3]: 107 

The Mir Core Module, along with the rest of the station, re-entered and burned up over the Pacific Ocean on March 23rd, 2001.

See also

References

  1. ^ "35 Years Ago: Launch of Mir Space Station's First Module - NASA". 2021-02-22. Retrieved 2026-05-22.
  2. ^ a b "Mir FAQs - Facts and history". www.esa.int. Retrieved 2026-05-22.
  3. ^ a b c d e f g h i j David Portree (1995). "Mir Hardware Heritage" (PDF). Archived from the original (PDF) on 2009-09-07.
  4. ^ "Soviet space programme: Philipp Meuser lifts the lid on the seminal cosmic design of Galina Balashova". July 2015.
  5. ^ "Spaceflight mission report: Soyuz T-15". www.spacefacts.de. Retrieved 2026-05-22.
  6. ^ a b McDonald, Sue (1998). "Mir Mission Chronicle" (PDF). ston.jsc.nasa.gov. Archived from the original (PDF) on 2009-07-30. Retrieved 2026-05-22.

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