Soyuz TM-16

Soyuz TM-16
Operator Rosaviakosmos
Mission duration 179 days, 43 minutes, 45 seconds
Orbits completed ~2,790
Spacecraft properties
Spacecraft type Soyuz-TM
Manufacturer NPO Energia
Launch mass 7,150 kilograms (15,760 lb)
Crew
Crew size 2 up
3 down
Members Gennadi Manakov
Alexander Poleshchuk
Landing Jean-Pierre Haigneré
Callsign Вулка́н (Vulkan - Volcano)
Start of mission
Launch date January 24, 1993, 05:58:05 (1993-01-24UTC05:58:05Z) UTC
Rocket Soyuz-U2
End of mission
Landing date July 22, 1993, 06:41:50 (1993-07-22UTC06:41:51Z) UTC
Landing site 140 kilometres (87 mi) S of Dzhezkazgan
Orbital parameters
Reference system Geocentric
Regime Low Earth
Perigee 393 kilometres (244 mi)
Apogee 394 kilometres (245 mi)
Inclination 51.6 degrees
Docking with Mir


Soyuz programme
(Manned missions)
 Soyuz TM-15 Soyuz TM-17

The Soyuz-TM crew transports (T - транспортный - Transportnyi - meaning transport, M - модифицированный - Modifitsirovannyi- meaning modified) were fourth generation (1986–2002) Soyuz spacecraft used for ferry flights to the Mir and ISS space stations. It added to the Soyuz-T new docking and rendezvous, radio communications, emergency and integrated parachute/landing engine systems. The new Kurs rendezvous and docking system permitted the Soyuz-TM to maneuver independently of the station, without the station making "mirror image" maneuvers to match unwanted translations introduced by earlier models' aft-mounted attitude control.

Soyuz TM-16 was the sixteenth expedition to the Russian Space Station Mir.[1]

Crew

Position Launching crew Landing crew
Commander Russia Gennadi Manakov
Second spaceflight
Flight Engineer Russia Alexander Poleshchuk
First spaceflight
Research Cosmonaut None France Jean-Pierre Haigneré
First spaceflight

Mission highlights

Soyuz TM-16 shown with the APAS-89 docking mechanism
APAS-89

16th expedition to Mir.

First Soyuz without a probe and drogue docking system since 1976. It carried an APAS-89 androgynous docking unit different from the APAS-75 unit used for ASTP in 1975, yet similar in general principles. Soyuz-TM 16 used it to dock with an androgynous docking port on the Kristall module. This was a test of the docking system in preparation for dockings by the Space Shuttles with Mir.

References


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