|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:communicationEquipment
|
S-band
|
|
gptkbp:crew
|
Yes
|
|
gptkbp:crewCapacity
|
3
Yes
|
|
gptkbp:crewSize
|
gptkb:Chinese_astronauts
|
|
gptkbp:designedBy
|
gptkb:China
|
|
gptkbp:diameter
|
2.8 m
|
|
gptkbp:diedIn
|
Yes
|
|
gptkbp:firstAppearance
|
gptkb:Shenzhou_9
|
|
gptkbp:firstAwarded
|
gptkb:Liu_Yang
|
|
gptkbp:firstFlight
|
gptkb:Shenzhou_5
1999
|
|
gptkbp:firstHomePort
|
Yes
|
|
gptkbp:futurePlans
|
expand crewed missions
|
|
gptkbp:hasPartnershipsWith
|
Yes
|
|
gptkbp:historicalResearch
|
Yes
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Shenzhou series
|
|
gptkbp:internationalCooperation
|
Yes
|
|
gptkbp:landingGear
|
parachute
|
|
gptkbp:launched
|
1-2 per year
|
|
gptkbp:launchSite
|
gptkb:Taiyuan_Satellite_Launch_Center
gptkb:Wenchang_Space_Launch_Site
gptkb:Jiuquan_Satellite_Launch_Center
approximately 20,000 kg
|
|
gptkbp:launchVehicle
|
Long March 2F
|
|
gptkbp:length
|
9.25 m
|
|
gptkbp:manufacturer
|
gptkb:China_Aerospace_Corporation
|
|
gptkbp:mission
|
gptkb:Shenzhou_7
based_on_Soyuz
multi-module_spacecraft
|
|
gptkbp:missions
|
gptkb:Beijing
up to 30 days
|
|
gptkbp:notableFeature
|
gptkb:Shenzhou_15
gptkb:Shenzhou_13
gptkb:Shenzhou_9
gptkb:Shenzhou_11
gptkb:Shenzhou_12
gptkb:Shenzhou_14
gptkb:Shenzhou_10
|
|
gptkbp:numberOfFigures
|
over 15
|
|
gptkbp:operatedBy
|
gptkb:China_National_Space_Administration
|
|
gptkbp:orbitalInclination
|
Yes
200-400 km
42 degrees
|
|
gptkbp:payloadCapacity
|
up to 1,000 kg
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:productionCompany
|
1992
|
|
gptkbp:purpose
|
crewed space missions
|
|
gptkbp:reliability
|
No
|
|
gptkbp:respondsTo
|
Yes
|
|
gptkbp:safetyFeatures
|
High
|
|
gptkbp:scientificName
|
Yes
|
|
gptkbp:secondaryMission
|
gptkb:Shenzhou_16
|
|
gptkbp:services
|
service module
|
|
gptkbp:successor
|
nan
|
|
gptkbp:technology
|
Yes
|
|
gptkbp:towingCapacity
|
Yes
|
|
gptkbp:weight
|
approximately 7,800 kg
|