|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:crew
|
gptkb:Oleg_Kononenko
gptkb:Satoshi_Furukawa
gptkb:Andrey_Babkin
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:descent_angle
|
approximately 30 degrees
|
|
gptkbp:descent_module_dimensions
|
2.2 m diameter
|
|
gptkbp:descent_module_material
|
aluminum alloy
|
|
gptkbp:descent_module_weight
|
approximately 2,500 kg
|
|
gptkbp:first_flight
|
TMA-21
|
|
gptkbp:homeworld
|
gptkb:Earth
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz TMA-21 descent module
|
|
gptkbp:landing_distance
|
at 10,000 feet
|
|
gptkbp:landing_site
|
gptkb:Kazakhstan
September 16, 2011
|
|
gptkbp:launch_date
|
April 5, 2011
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz_FG
|
|
gptkbp:launched
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mission
|
gptkb:Soyuz_TMA-21_patch
|
|
gptkbp:mission_duration
|
159 days
|
|
gptkbp:mission_type
|
gptkb:human_spaceflight
|
|
gptkbp:module
|
gptkb:navigation_system
gptkb:cybernetic_enhancements
gptkb:monitor
gptkb:parachute
gptkb:health_services
gptkb:Control
gptkb:safety_standards
gptkb:safety_equipment
gptkb:gasoline
gptkb:Team_Rocket
gptkb:communication_systems
gptkb:handbags
gptkb:sensors
environmental control system
control surfaces
power system
about 3 hours
data recording system
thermal protection system
approximately 7.5 km/s
stabilization system
recovery system
emergency system
ballistic descent
Soyuz TMA-21 orbital module
instrumentation system
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:part_of
|
Soyuz TMA-21 mission
|
|
gptkbp:predecessor
|
gptkb:Soyuz_TMA-20
|
|
gptkbp:service
|
Soyuz TMA-21 service module
|
|
gptkbp:speed
|
controlled descent
|
|
gptkbp:successor
|
gptkb:Soyuz_TMA-22
|
|
gptkbp:touchdown
|
soft landing
|
|
gptkbp:used_for
|
transporting astronauts
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_TMA-21
|
|
gptkbp:bfsLayer
|
6
|