Properties (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:spacecraft
|
| gptkbp:controls |
automatic and manual
|
| gptkbp:crew |
yes
|
| gptkbp:crew_size |
3
|
| gptkbp:diameter |
2.2 m
|
| gptkbp:duration |
up to 180 days
|
| gptkbp:firstFlight |
2002
2017 |
| gptkbp:height |
2.5 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Soyuz TMA Descent Module
|
| gptkbp:landingGear |
parachute
|
| gptkbp:launchSite |
Baikonur Cosmodrome
|
| gptkbp:launchVehicle |
gptkb:Soyuz_rocket
|
| gptkbp:manufacturer |
gptkb:Russian_Federal_Space_Agency
|
| gptkbp:material |
phenolic resin
|
| gptkbp:maximum_speed |
28,000 km/h
|
| gptkbp:maxTakeoffWeight |
7,200 kg
|
| gptkbp:missions |
16
|
| gptkbp:operational_area |
gptkb:Kazakhstan
|
| gptkbp:operational_status |
retired
|
| gptkbp:operationalHistory |
2002
|
| gptkbp:orbitalInclination |
gptkb:Soyuz_TMA_Orbital_Module
|
| gptkbp:purpose |
transport_crew_to_and_from_the_International_Space_Station
|
| gptkbp:service_area |
gptkb:Soyuz_TMA_Service_Module
|
| gptkbp:succeededBy |
100%
|
| gptkbp:youth_development |
ballistic and guided
|