|
gptkbp:instanceOf
|
space station
|
|
gptkbp:aircraft
|
single module
|
|
gptkbp:communicationEquipment
|
S-band
|
|
gptkbp:country
|
gptkb:China
|
|
gptkbp:crew
|
multiple missions
conducted for astronauts
|
|
gptkbp:crewCapacity
|
3
|
|
gptkbp:decommissioningDate
|
March 2012
|
|
gptkbp:dimensions
|
2.4 m diameter
|
|
gptkbp:firstAwarded
|
probe and drogue
|
|
gptkbp:hasPartnershipsWith
|
none
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Tiangong-7
|
|
gptkbp:internationalCooperation
|
limited
|
|
gptkbp:launchDate
|
September 29, 2011
|
|
gptkbp:launched
|
successful
September 2011
|
|
gptkbp:launchSite
|
gptkb:Jiuquan_Satellite_Launch_Center
8,000 kg
|
|
gptkbp:launchVehicle
|
Long March 2F
|
|
gptkbp:length
|
10.5 m
|
|
gptkbp:lifespan
|
approximately 2 years
|
|
gptkbp:manufacturer
|
gptkb:China_Academy_of_Space_Technology
|
|
gptkbp:mission
|
Low Earth Orbit
cylindrical
decommissioned
modular space station
|
|
gptkbp:missions
|
gptkb:Beijing_Aerospace_Control_Center
|
|
gptkbp:operationalStatus
|
5 months
decommissioned
|
|
gptkbp:orbitalInclination
|
90 minutes
340 km
42.8 degrees
|
|
gptkbp:payloadCapacity
|
1,000 kg
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:purpose
|
testing technologies for future space stations
|
|
gptkbp:renovated
|
splashdown
|
|
gptkbp:researchFocus
|
microgravity research
|
|
gptkbp:respondsTo
|
controlled
|
|
gptkbp:scientificName
|
various
conducted
|
|
gptkbp:secondaryMission
|
gptkb:Shenzhou_8
gptkb:Shenzhou_9
|
|
gptkbp:services
|
experimental space module
|
|
gptkbp:successor
|
gptkb:Tiangong_program
Tiangong-8
|
|
gptkbp:totalGoals
|
15 m³
|
|
gptkbp:weight
|
8,000 kg
|