|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:communicationEquipment
|
high-frequency radio
|
|
gptkbp:controls
|
autonomous and manual
|
|
gptkbp:coolingSystem
|
carbon phenolic resin
|
|
gptkbp:crew
|
extensive
|
|
gptkbp:crewCapacity
|
3
Yes
|
|
gptkbp:designedBy
|
gptkb:China_National_Space_Administration
|
|
gptkbp:developer
|
2003
|
|
gptkbp:diedIn
|
Yes
|
|
gptkbp:dimensions
|
2.5 m diameter
|
|
gptkbp:environmentalImpact
|
Yes
|
|
gptkbp:firstFlight
|
gptkb:Shenzhou_1
gptkb:Shenzhou_15
gptkb:Shenzhou_5
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Shenzhou reentry capsule
|
|
gptkbp:inspiration
|
Chinese_space_exploration
|
|
gptkbp:internationalCooperation
|
limited
|
|
gptkbp:landingGear
|
parachute
|
|
gptkbp:launched
|
approximately 1-2 per year
|
|
gptkbp:launchSite
|
gptkb:Jiuquan_Satellite_Launch_Center
|
|
gptkbp:launchVehicle
|
Long March 2F
|
|
gptkbp:mission
|
manned spaceflight
|
|
gptkbp:navigationEquipment
|
inertial navigation
|
|
gptkbp:notableFeature
|
gptkb:Shenzhou_7
gptkb:Shenzhou_15
gptkb:Shenzhou_13
gptkb:Shenzhou_9
gptkb:Shenzhou_11
gptkb:Shenzhou_12
gptkb:Shenzhou_14
gptkb:Shenzhou_10
gptkb:Shenzhou_6
|
|
gptkbp:operationalStatus
|
2003
|
|
gptkbp:orbitalInclination
|
Yes
|
|
gptkbp:payloadCapacity
|
up to 100 kg
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:productionCompany
|
1999
|
|
gptkbp:renovated
|
gptkb:Inner_Mongolia
|
|
gptkbp:safetyFeatures
|
good
|
|
gptkbp:scientificName
|
Yes
|
|
gptkbp:secondaryMission
|
planned
|
|
gptkbp:services
|
Yes
|
|
gptkbp:speed
|
up to 28,000 km/h
|
|
gptkbp:succeededBy
|
high
|
|
gptkbp:technology
|
communication technology
life support technology
reentry technology
thermal protection technology
navigation_technology
|
|
gptkbp:usedIn
|
gptkb:Shenzhou_program
|
|
gptkbp:weight
|
approximately 2,500 kg
|