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gptkbp:instance_of
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gptkb:spacecraft
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gptkbp:crew
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gptkb:Dmitry_Kondratyev
gptkb:3
gptkb:Catherine_Coleman
gptkb:Shannon_Walker
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gptkbp:crew_capacity
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gptkb:3
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gptkbp:descent_module_color
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gptkb:white
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gptkbp:descent_module_design
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ballistic
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gptkbp:descent_module_diameter
|
2.2 m
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|
gptkbp:descent_module_function
|
crew return
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gptkbp:descent_module_length
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2.5 m
|
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gptkbp:descent_module_material
|
aluminum alloy
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gptkbp:descent_module_weight
|
2,500 kg
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz TMA-29 descent module
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gptkbp:landing_site
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gptkb:Kazakhstan
March 16, 2011
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gptkbp:launch_date
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December 21, 2010
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gptkbp:launch_site
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gptkb:Baikonur_Cosmodrome
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gptkbp:launched
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gptkb:Soyuz-FG_rocket
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mission_duration
|
92 days
|
|
gptkbp:mission_type
|
gptkb:human_spaceflight
|
|
gptkbp:module
|
gptkb:cybernetic_enhancements
gptkb:parachute
gptkb:safety_equipment
gptkb:gasoline
gptkb:navigation
gptkb:communication
gptkb:sensors
gptkb:power_adapter
propulsion
airbags
safety systems
monitoring
control surfaces
control
telemetry
stabilization
life support
thermal protection
recovery
emergency systems
data handling
crew interface
ballistic recovery system
emergency parachute
environment control
|
|
gptkbp:orbital_period
|
90 minutes
|
|
gptkbp:part_of
|
Soyuz TMA-29 mission
|
|
gptkbp:predecessor
|
gptkb:Soyuz_TMA-28
|
|
gptkbp:speed
|
7.5 km/s
|
|
gptkbp:successor
|
gptkb:Soyuz_TMA-30
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_TMA-29
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|
gptkbp:bfsLayer
|
6
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