The deorbit was carried out in three stages. The first stage was waiting for atmospheric drag to decay the orbit to an average of 220 kilometres (140 mi). This began with the docking of Progress M1-5. The second stage was the transfer of the station into a 165-by-220-kilometre (103 mi × 137 mi) orbit. This was achieved with two burns of the Progress M1-5's control engines at 00:32 UTC and 02:01 UTC on 23 March 2001. After a two-orbit pause, the third and final stage of Mir's deorbit began with the firing of Progress M1-5's control engines and main engine at 05:08 UTC, lasting a little over 22 minutes. The atmospheric entry at the altitude of 100 kilometres (62 mi) occurred at 05:44 UTC near Nadi, Fiji.[2]
Background
Mir three years before deorbit
After the construction of the International Space Station began in 1998, Russian resources were split between the two stations.[3][4][5] In 2000, Roscosmos signed an agreement with MirCorp to lease the station for commercial use,[6] with the Soyuz TM-30 mission, intended to prepare the station for future use and conduct some commercial research, being flown later that year.[7][self-published source] This was to have been followed by more missions, including flights with space tourists. Due to the Russian government being concerned about MirCorp's ability to fund these missions, Roscosmos decided against funding the continued operation of Mir.[3][4]
In November 2000, Roscosmos decided to deorbit Mir,[8] and the next month Russian Prime MinisterMikhail Kasyanov signed an order to do so.[9] By this stage Mir was well past the end of its design life,[10] and Roscosmos General Director Yuri Koptev believed that "any of its systems could well fail at any time".[8] Therefore, it was decided to deorbit it while it was still functioning rather than risk it falling back to Earth out of control, like Skylab in 1979[11] and Salyut 7 in 1991, potentially dropping debris over a populated area.[4]
The Mir Deorbit Monitoring Group, whose members were located in the Russian Mission Control Center (RMCC) and ESOC, was monitoring the whole dynamic phase of operation. Both RMCC control rooms in Moscow were used for the massive media presence during the final stages of operation.[12] Real-time reports from RMCC were provided via teleconference during each deorbit burn to ESA spokespersons and representatives from national agencies. Video transmissions from RMCC were also made available to ESOC.[citation needed]
Two out of three Progress M1-5 propulsion firings, at approximately 90 minute intervals, were used to bring the perigee of Mir down to an altitude of 160 kilometres (99 mi) above the Earth's surface.[13][self-published source] A tough contact with the atmosphere occurred at 100 kilometres (62 mi) altitude, when some of the external light elements of Mir were torn off due to the rush through the rarefied air.[13] At an altitude of 90 kilometres (56 mi) sufficient heating from Mir's hull created a glowing halo of hot plasma.[13][self-published source] At about that time, the orbital complex broke apart and several of Mir's elements, surrounded by the plasma, were visible from Fiji against the evening sky.[13][self-published source] Television pictures were transmitted around the world within a few minutes of the event.[13][self-published source] The entire process lasted from about 16:20 to 20:29 local solar time. A short press conference was held in RMCC to cover the final stage of deorbit.[citation needed]
At the time, Mir was the largest spacecraft ever to reenter the Earth's atmosphere, and there were concerns that sizeable pieces of debris, particularly from the docking assemblies, gyrodynes and external structure, could survive reentry.[17] Amid debris fall, New Zealand issued international warnings to ships and aircraft traveling in the South Pacific area.[18] Deputy director of New Zealand's Maritime Safety Authority, Tony Martin, said that the chances of debris hitting ships would be very small.[18] A similar situation occurred in Japan, whose residents were warned to stay indoors during the forty-minute period when debris were most likely to fall. The local officials admitted that the chances of an accident were very low.[18] The location of Mir announced after re-entry was 40°S160°W / 40°S 160°W / -40; -160 (Mir impact site) in the South Pacific Ocean. The debris spread about ±1,500 kilometres (930 mi) along track and ±100 kilometres (62 mi) laterally, reduced from the earlier estimate due to the steeper re-entry angle.[13]
^Paul, Scott D (2002). "NASA JSC trajectory operational support for entry of Space Station MIR". Harvard University. Bibcode:2002ESASP.498...41P.
^Böckstiegel, Karl-Heinz (1995). "A.IX.3.1.2". Space Law. Kluwer Law International. ISBN0-7923-0091-2. Archived from the original on 17 July 2017. Retrieved 27 September 2016.
