Soyuz TM-16
| Operator | Rosaviakosmos | ||||
|---|---|---|---|---|---|
| COSPAR ID | 1993-005A | ||||
| 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 UTC | ||||
| Rocket | Soyuz-U2 | ||||
| End of mission | |||||
| Landing date | July 22, 1993, 06:41:50 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 | |||||
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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 | Second spaceflight | |
| Flight Engineer | First spaceflight | |
| Research Cosmonaut | None | First spaceflight |
Mission highlights


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
- ↑ The mission report is available here:http://www.spacefacts.de/mission/english/soyuz-tm16.htm


