|
gptkbp:instance_of
|
gptkb:space_station
|
|
gptkbp:capacity
|
15 m³
|
|
gptkbp:collaboration
|
limited international cooperation
|
|
gptkbp:collaborations
|
partnerships with research institutions
collaborated with universities
|
|
gptkbp:communication_system
|
solar power system
high-speed communication system
|
|
gptkbp:control_system
|
advanced control system
|
|
gptkbp:country
|
gptkb:China
|
|
gptkbp:crew
|
extensive crew training programs
2 crew members during missions
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:design
|
2 years
|
|
gptkbp:docking_system
|
automatic docking system
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Tiangong 3
|
|
gptkbp:international_visibility
|
increased international visibility for China
|
|
gptkbp:is_explored_in
|
part of China's space exploration efforts
|
|
gptkbp:launch_date
|
gptkb:2013
April 2013
|
|
gptkbp:launch_event
|
successful launch
|
|
gptkbp:launch_mass
|
8,600 kg
|
|
gptkbp:launch_site
|
gptkb:Jiuquan_Satellite_Launch_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Long_March_2_F
|
|
gptkbp:launched
|
1 launch
|
|
gptkbp:mass
|
8,600 kg
|
|
gptkbp:mission
|
conducted spacewalks during missions
to test technologies for future space stations
|
|
gptkbp:mission_duration
|
approximately 20 days
|
|
gptkbp:module
|
experimental space laboratory
|
|
gptkbp:module_diameter
|
3.35 m
|
|
gptkbp:module_length
|
10.4 m
|
|
gptkbp:operational_status
|
decommissioned
|
|
gptkbp:operator
|
gptkb:China_National_Space_Administration
|
|
gptkbp:orbit_type
|
low Earth orbit
|
|
gptkbp:orbital_inclination
|
42 degrees
|
|
gptkbp:orbital_period
|
approximately 90 minutes
|
|
gptkbp:payload_capacity
|
up to 1,000 kg
|
|
gptkbp:predecessor
|
gptkb:Tiangong_2
|
|
gptkbp:recovery_method
|
controlled reentry
|
|
gptkbp:research
|
various scientific experiments
|
|
gptkbp:research_areas
|
biological and physical sciences
|
|
gptkbp:research_focus
|
microgravity research
|
|
gptkbp:scientific_instruments
|
various scientific instruments
|
|
gptkbp:spacecraft
|
gptkb:spacecraft
modular design
operated in low Earth orbit.
various spacecraft components
|
|
gptkbp:speed
|
reentered Earth's atmosphere in 2016
|
|
gptkbp:successor
|
gptkb:Tiangong_program
gptkb:Tiangong_4
|
|
gptkbp:sustainability
|
two solar arrays
|
|
gptkbp:was_a_demonstration_of
|
demonstrated space technologies
|
|
gptkbp:bfsParent
|
gptkb:Chinese_space_program
gptkb:Tiangong_2
|
|
gptkbp:bfsLayer
|
6
|