|
gptkbp:instanceOf
|
space station
|
|
gptkbp:aircraft
|
10.4 m
3.35 m
|
|
gptkbp:cockpit
|
APAS compatible
|
|
gptkbp:communicationEquipment
|
S-band and Ku-band
|
|
gptkbp:country
|
gptkb:China
|
|
gptkbp:crew
|
2
3
|
|
gptkbp:crewCapacity
|
3
|
|
gptkbp:firstAwarded
|
APAS
|
|
gptkbp:height
|
3.35 m
|
|
gptkbp:historicalResearch
|
microgravity experiments
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Tiangong-20
|
|
gptkbp:internationalCooperation
|
limited
|
|
gptkbp:launchDate
|
2016-09-15
|
|
gptkbp:launched
|
2
3
successful
|
|
gptkbp:launchSite
|
gptkb:Jiuquan_Satellite_Launch_Center
8,600 kg
|
|
gptkbp:launchVehicle
|
Long March 2F
|
|
gptkbp:length
|
10.4 m
|
|
gptkbp:manufacturer
|
gptkb:China_Academy_of_Space_Technology
|
|
gptkbp:mission
|
crewed
decommissioned
8,600 kg
15 m³
Long March 2F rocket
modular space station
cylindrical module
low_Earth_orbit
|
|
gptkbp:missionCapabilities
|
controlled descent
|
|
gptkbp:missions
|
30 days
|
|
gptkbp:operationalStatus
|
2016-2017
retired
|
|
gptkbp:orbitalInclination
|
90 minutes
340 km
42.8 degrees
|
|
gptkbp:payloadCapacity
|
1,000 kg
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:predecessor
|
Tiangong-19
|
|
gptkbp:propulsion
|
2 kW
|
|
gptkbp:releaseYear
|
2017-04-19
|
|
gptkbp:renovated
|
controlled reentry
|
|
gptkbp:researchFocus
|
space technology
|
|
gptkbp:respondsTo
|
gptkb:Shenzhou_spacecraft
|
|
gptkbp:scientificName
|
microgravity research
technology demonstration
|
|
gptkbp:secondaryMission
|
gptkb:Shenzhou_11
|
|
gptkbp:services
|
experimental space laboratory
|
|
gptkbp:squadrons
|
S-band, Ku-band
|
|
gptkbp:successor
|
gptkb:Tiangong_program
Tiangong-21
|
|
gptkbp:weight
|
8,600 kg
|
|
gptkbp:width
|
3.35 m
|