|
gptkbp:instance_of
|
gptkb:spacecraft
gptkb:Soyuz_spacecraft
|
|
gptkbp:capacity
|
10.5 m³
|
|
gptkbp:communication
|
S-band
|
|
gptkbp:communication_system
|
S-band
|
|
gptkbp:control_system
|
Fly-by-wire system
|
|
gptkbp:cooling_system
|
Heat shield
|
|
gptkbp:crew
|
gptkb:Soyuz-FG
gptkb:Soyuz_capsule
gptkb:Oleg_Kononenko
gptkb:Japanese
gptkb:3
gptkb:Kazakhstan
gptkb:Oleg_Artemyev
gptkb:Alexander_Gerst
gptkb:Scott_Kelly
gptkb:Andrey_Babkin
gptkb:Kimiya_Yui
gptkb:American
gptkb:Russian
gptkb:Yes
gptkb:launch_escape_system
3,000 kg
2015-09-11
2016-02-18
2015-07-23
Soyuz TMA-95 capsule
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:crew_return_type
|
parachute landing
|
|
gptkbp:crew_return_vehicle_design
|
gptkb:Soyuz_TMA
|
|
gptkbp:crew_return_vehicle_landing_date
|
2016-02-18
|
|
gptkbp:crew_return_vehicle_landing_site
|
gptkb:Kazakhstan
|
|
gptkbp:crew_return_vehicle_launch_date
|
2015-07-23
|
|
gptkbp:crew_return_vehicle_manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:crew_return_vehicle_mass
|
2,500 kg
|
|
gptkbp:crew_return_vehicle_status
|
retired
|
|
gptkbp:date
|
2016-02-18
|
|
gptkbp:debut
|
2021-04-23
2002-11-20
|
|
gptkbp:docking_system
|
gptkb:APAS
|
|
gptkbp:duration
|
52 days
|
|
gptkbp:first_flight
|
gptkb:2003
gptkb:2017
gptkb:Soyuz_MS-18
gptkb:Soyuz_TMA-1
TMA-95
|
|
gptkbp:flight_style
|
gptkb:10
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz TMA-95
|
|
gptkbp:is_a_destination_for
|
gptkb:International_Space_Station
|
|
gptkbp:landing_site
|
gptkb:Kazakhstan
2015-09-11
|
|
gptkbp:launch_date
|
10:00 UTC
2015-07-23
|
|
gptkbp:launch_mass
|
7,200 kg
9,500 kg
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz-FG
|
|
gptkbp:launch_window
|
2015-07-23 to 2015-07-25
|
|
gptkbp:life_support_system
|
gptkb:Yes
Closed-loop system
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mass
|
7,200 kg
|
|
gptkbp:mission
|
gptkb:Ts_UP-Moscow
gptkb:Soyuz_TMA-95_patch
Completed
ISS crew rotation
|
|
gptkbp:mission_duration
|
52 days
approximately 5 months
|
|
gptkbp:mission_type
|
Crewed
crewed mission
|
|
gptkbp:module
|
gptkb:Soyuz_spacecraft
gptkb:Lunar_Module
gptkb:Public_service
|
|
gptkbp:navigation_system
|
Inertial navigation system
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:operator
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:payload_capacity
|
2.5 m
2.2 m
7.2 m
7,200 kg
100 kg to ISS
|
|
gptkbp:power_source
|
Solar panels
solar panels
|
|
gptkbp:predecessor
|
gptkb:Soyuz_TMA-94
|
|
gptkbp:propulsion
|
Hypergolic
|
|
gptkbp:related_vehicle
|
gptkb:Soyuz_capsule
|
|
gptkbp:service
|
gptkb:Yes
|
|
gptkbp:spacecraft
|
gptkb:Soyuz_TMA
|
|
gptkbp:speed
|
gptkb:Yes
7.5 km/s
|
|
gptkbp:successor
|
gptkb:Soyuz_MS-01
|
|
gptkbp:team
|
gptkb:Yes
|
|
gptkbp:bfsParent
|
gptkb:Michael_E._Lopez-Alegria
|
|
gptkbp:bfsLayer
|
5
|