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Soyuz TM-2


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Soyuz TM-2

COSPAR ID
1987-013A
SATCAT no.

17482
Mission duration
174 days, 3 hours, 25 minutes, 56 seconds
Orbits completed
~2,810


Spacecraft properties
Spacecraft type
Soyuz-TM
Manufacturer
NPO Energia
Launch mass
7,100 kilograms (15,700 lb)


Crew
Crew size
2 up
3 down
Members
Aleksandr Laveykin
Launching
Yuri Romanenko
Landing
Aleksandr Viktorenko
Muhammed Faris
Callsign
Taimyr


Start of mission
Launch date
5 February 1987, 21:38:16 (1987-02-05UTC21:38:16Z) UTC[1]
Rocket
Soyuz-U2
Launch site
Baikonur 1/5


End of mission
Landing date
30 July 1987, 01:04:12 (1987-07-30UTC01:04:13Z) UTC[2]
Landing site
80 kilometres (50 mi) from Arkalyk


Orbital parameters
Reference system
Geocentric
Regime
Low Earth
Perigee
341 kilometres (212 mi)
Apogee
365 kilometres (227 mi)
Inclination
51.6 degrees
Period
91.6 minutes


Docking with Mir



Soyuz programme
(Manned missions)


← Soyuz T-15


Soyuz TM-3 →



Soyuz TM-2 was the spacecraft used to launch a long duration crew to the Soviet space station Mir, which was unmanned at the time. TM-2 was launched in February 1987, and it was first manned spaceflight of the Soyuz-TM spacecraft,[3] and the second manned spaceflight to Mir (the first being Soyuz T-15). The crew of the long duration expedition, Mir EO-2, who were launched by TM-2 consisted of Soviet cosmonauts Yuri Romanenko and Aleksandr Laveykin.


The spacecraft remained docked to Mir, functioning as a lifeboat for the EO-2 crew, until July 1987 when it returned to Earth carrying Laveykin and the two man crew of Mir EP-1. Romanenko later returned to Earth in Soyuz TM-3 at the end of EO-2.




Contents






  • 1 Crew


  • 2 Mission parameters


  • 3 Mission highlights


  • 4 References





Crew[edit]



























Position
Launching crew
Landing crew
Commander

Soviet Union Yuri Romanenko
Mir EO-2
Third and last spaceflight

Soviet Union Aleksandr Viktorenko
Mir EP-1
First spaceflight
Flight Engineer

Soviet Union Aleksandr Laveykin
Mir EO-2
Only spaceflight
Research Cosmonaut
None

Syria Muhammed Faris
Mir EP-1
Only spaceflight


Mission parameters[edit]




  • Mass: 7100 kg


  • Perigee: 341 km


  • Apogee: 365 km


  • Inclination: 51.6°


  • Period: 91.6 minutes



Mission highlights[edit]



Early in the expedition EO-2, the module Kvant-1 was launched to automatically dock with Mir. The docking system, known as the "Igla system", was not behaving as expected. On April 5 the EO-2 crew retreated to the Soyuz TM-2 spacecraft so that they could escape in the event the module got out of control. About 200 m out, the docking system lost its lock on Mir’s aft port antenna. The cosmonauts watched from within Soyuz-TM 2 as the Kvant/ FSM combination passed within 10 m of the station.[1] Following an emergency spacewalk, Kvant fully docked to the station on April 11.



References[edit]





  1. ^ ab "Mir EO-2". Encyclopedia Astronautica. Archived from the original on 9 April 2007. Retrieved 11 November 2010..mw-parser-output cite.citation{font-style:inherit}.mw-parser-output q{quotes:"""""""'""'"}.mw-parser-output code.cs1-code{color:inherit;background:inherit;border:inherit;padding:inherit}.mw-parser-output .cs1-lock-free a{background:url("//upload.wikimedia.org/wikipedia/commons/thumb/6/65/Lock-green.svg/9px-Lock-green.svg.png")no-repeat;background-position:right .1em center}.mw-parser-output .cs1-lock-limited a,.mw-parser-output .cs1-lock-registration a{background:url("//upload.wikimedia.org/wikipedia/commons/thumb/d/d6/Lock-gray-alt-2.svg/9px-Lock-gray-alt-2.svg.png")no-repeat;background-position:right .1em center}.mw-parser-output .cs1-lock-subscription a{background:url("//upload.wikimedia.org/wikipedia/commons/thumb/a/aa/Lock-red-alt-2.svg/9px-Lock-red-alt-2.svg.png")no-repeat;background-position:right .1em center}.mw-parser-output .cs1-subscription,.mw-parser-output .cs1-registration{color:#555}.mw-parser-output .cs1-subscription span,.mw-parser-output .cs1-registration span{border-bottom:1px dotted;cursor:help}.mw-parser-output .cs1-hidden-error{display:none;font-size:100%}.mw-parser-output .cs1-visible-error{font-size:100%}.mw-parser-output .cs1-subscription,.mw-parser-output .cs1-registration,.mw-parser-output .cs1-format{font-size:95%}.mw-parser-output .cs1-kern-left,.mw-parser-output .cs1-kern-wl-left{padding-left:0.2em}.mw-parser-output .cs1-kern-right,.mw-parser-output .cs1-kern-wl-right{padding-right:0.2em}


  2. ^ "Mir EP-1". Encyclopedia Astronautica. Archived from the original on 29 November 2010. Retrieved 11 November 2010.


  3. ^ "Soyuz TM". Encyclopedia Astronautica. Retrieved 11 November 2010.















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