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International station MIR
Earlier events and reports on Mir can be found here . Milestones and Events
Mir ConfigurationThe Mir Complex (satellite catalog number 16609/ International Designation 86017A) was launched on the 19th of February, 1986, replacing the successful Salyut series of space stations run by the Soviets throughout the 1970's and 1980's. Operating in an orbit some 390 km high, inclined at 51.6 degrees (the optimum launch direction from the Baikonur (Tyuratam) Cosmodrome is north of east to avoid flying through Chinese air-space), the space station is modular in design and has been slowly constructed in such a manner. The crew in TM-1 first occupied Mir on March 14, 1986. With the exception of EVAs/or moving the Soyuz from one docking port to another, Mir has been un-occupied only on four occasions. The Mir 1 Crew left Mir on May 5, 1986 for Salyut 7.
Sources: David S. F. Portree and David HarlandSpaceviews has views and information on the various modules of Mir. Individual diagrams of the various modules and vehicles can be found at the Mir '97 website. Mir Core ModuleThe Mir complex consists of the original core Mir core module (dimensions 15 x 4.15 m, mass about 20000 kg) that was launched in Feb 19, 1986. It provides the basic services of living quarters, life support, power and thermal control. KvantAt the rear axial port of Mir (on the +x axis) is docked the Kvant(17845/87030A) astrophysics module (5.8 x 4.15 m, 11000 kg) which was launched on 31st March, 1987. This second module is technically known as Kvant, but is identified in some resources as Kvant 1 so as not to confuse it with the later Kvant 2 module. The Kvant module houses the Roentgen astrophysics observatory with the Pulsar x-ray telescopes, a gamma ray detector and the Glazar UV telescope. Also mounted on this module is the Sofora mast structure, 14 meters long, with an roll control thruster package at one end. The pitch and yawl attitude of Mir is maintained by gyrodynes. A rear axial docking port (on the +x axis) of Kvant is used to accommodate the arrival of either a Progress-M or Soyuz-TM vehicle. The Progress M re-supply vehicle (7.5 x 2 m, 7000 kg) is capable of free-flight for extended periods. When a Soyuz docking takes place it is undocked either for a destructive re-entry or maintained in orbit. When the older docked Soyuz returns to Earth with the relieved crew, the Progress may be re-docked until relieved by another Progress vehicle. The Progress M uses solar arrays to charge its power supply system's batteries. While docked to the Mir, its engine can be used to maintain or alter the space station's orbit. In the early 1990's the Progress vehicle was equipped with a small return capsule called the Reentry Ballistic Capsule (VBK) (mounted to the forward docking hatch) to return material back to earth. In 1995 the use of this capsule seems to have been discontinued with the periodic docking of the Shuttle with resupplies to Mir. The expendable vehicle is loaded with any materials for disposal. The Progress-M separates to normally make a destructive re-entry over the South Pacific. The Soyuz-TM vehicle (7.5 x 2 m, 7000 kg) can deliver 2-3 cosmonauts to Mir depending upon what type Soyuz booster is used. It normally takes some 2-3 days to reach the space station and it is capable of remaining docked for up to 200 days prior to returning to Earth. Forward axial/radial docking (-x)portOn the forward end of the Mir core module (opposite the Kvant module) is the forward axial docking port that delineates the center of the (-x) axis. On this docking port either a Progress or Soyuz vessel is docked. The four radial (side) ports on this forward module capture the four remaining modules on the y and z axis. Kvant 2On one of the side ports (+y axis) is docked the Kvant 2 (20335/89093A) module (12 x 4.4 m, 20000 kg) which was launched on the 26 November, 1989. This carries technical support facilities and amenities. It also houses the airlock which the Cosmonauts use to access the outside of the Mir complex in extravehicular activities (EVA). The airlock has also served as "home" to the visiting American astronaut as the Spektr module is no longer habitable. SpektrOn the opposing side port (-y axis) is the Spektr (23579/95024A) remote sensing module for geophysical sciences (12 x 4.35 m, 19,640 kg). It was launched on May 20, 1995 and arrived at Mir on June 1, 1995. Integral to the Spektr module was a planned robotic arm system that would be able to dispense/retrieve experiments located externally on Mir. The Pelican System is installed with the exception of the robotic master-slave arm. This module suffered solar array and hull damage on June 25, 1997 when Progress M-34 was being manually maneuvered from Mir to re-dock to the Kvant module. This module is presently depressurized and isolated from the remainder of the Mir complex. Modifications have been made to the Spektr hatch to allow power and control cable penetrations through the hatch, while still isolating Spektr from the remaining station. These modifications have allowed power generation to return to approximately 70% of the pre-collision conditions. KristallOn another side port (the -z axis) is the Kristall (20635/90048A) industrial processing module (12 x 4.4 m, 20000 kg). Launched 31 May 1990, this module is used for semiconductor and biological experiments. It also houses Earth observation instruments. Attached to the end of Kristall is the Mir/Shuttle docking moduledelivered by Atlantis on mission STS-74 on November 14, 1995. Thus, the Shuttle docks to Mir on the -z axis. PrirodaFinally, the Priroda (23848/96023A) remote sensing module (12 x 4.35 m, 19,700 kg) was launched on April 23, 1996, and resides at the final vacant side port on the +z axis. This module houses passive and active radiometers (IKAR), a synthetic aperture radar (Travers), an infra-red radiometer (Istok 1), a spectrometer for measuring ozone and aerosol concentrations (Ozon-M), visible and infra-red spectrometers (MOZ-Obzor), optical scanners (MSU-SK, MSU-E) and a device for remote interrogation of geophysical stations (Centaur). Thus, the present and final configuration of the Mir complex (32 m long, 30 m wide, 27 m high) is:
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