|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:collaboration
|
limited
|
|
gptkbp:communication_system
|
advanced
solar panels
|
|
gptkbp:control_system
|
automatic and manual
|
|
gptkbp:cooling_system
|
active and passive
|
|
gptkbp:crew
|
yes
extensive
implemented
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:design
|
10 years
|
|
gptkbp:designed_by
|
gptkb:China
|
|
gptkbp:development
|
gptkb:1992
|
|
gptkbp:durability
|
no
|
|
gptkbp:first_flight
|
gptkb:Shenzhou_1
gptkb:1999
gptkb:Shenzhou_16
gptkb:Shenzhou_5
|
|
gptkbp:future_plans
|
continued development
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Shenzhou series
|
|
gptkbp:inspiration
|
future missions
|
|
gptkbp:international_recognition
|
growing
|
|
gptkbp:landing_site
|
gptkb:Inner_Mongolia
|
|
gptkbp:launch_date
|
annual
|
|
gptkbp:launch_mass
|
approximately 7,800 kg
|
|
gptkbp:launch_site
|
gptkb:Jiuquan_Satellite_Launch_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Long_March_2_F
|
|
gptkbp:life_support_system
|
yes
|
|
gptkbp:mission
|
over 15
|
|
gptkbp:module
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:navigation_system
|
inertial navigation
|
|
gptkbp:notable_mission
|
gptkb:Shenzhou_15
gptkb:Shenzhou_16
gptkb:Shenzhou_13
gptkb:Shenzhou_9
gptkb:Shenzhou_11
gptkb:Shenzhou_12
gptkb:Shenzhou_14
gptkb:Shenzhou_10
|
|
gptkbp:operated_by
|
gptkb:China_National_Space_Administration
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:orbital_altitude
|
200-400 km
|
|
gptkbp:part_of
|
Chinese human spaceflight program
|
|
gptkbp:payload_capacity
|
2.5 m
up to 3,000 kg
9.25 m
|
|
gptkbp:purpose
|
gptkb:human_spaceflight
|
|
gptkbp:recovery_method
|
yes
|
|
gptkbp:research
|
conducted on board
|
|
gptkbp:service
|
yes
|
|
gptkbp:spacecraft
|
gptkb:spacecraft
|
|
gptkbp:speed
|
yes
|
|
gptkbp:successor
|
gptkb:Tiangong_program
|
|
gptkbp:bfsParent
|
gptkb:Shenzhou_11_mission
gptkb:China's_human_spaceflight_program
|
|
gptkbp:bfsLayer
|
7
|