|
gptkbp:instanceOf
|
crewed spacecraft
|
|
gptkbp:aircraft
|
2.5 m
2.8 m
Three-module design
9.25 m
|
|
gptkbp:communicationEquipment
|
S-band
|
|
gptkbp:crew
|
gptkb:Yang_Liwei
Yes
Commander
Extensive
|
|
gptkbp:crewCapacity
|
Chinese
First-time astronaut
|
|
gptkbp:crewSize
|
1
|
|
gptkbp:diedIn
|
Yes
|
|
gptkbp:duration
|
5 days
|
|
gptkbp:firstFlight
|
Yes
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Shenzhou 2
|
|
gptkbp:internationalClassification
|
Yes
|
|
gptkbp:internationalCooperation
|
Limited
|
|
gptkbp:landingGear
|
gptkb:Siberia
|
|
gptkbp:launchDate
|
2001-01-09
03:00 UTC
|
|
gptkbp:launched
|
Successful
|
|
gptkbp:launchSite
|
gptkb:Jiuquan_Satellite_Launch_Center
7,800 kg
|
|
gptkbp:launchVehicle
|
Long March 2F
|
|
gptkbp:mission
|
gptkb:Shenzhou
gptkb:China_Aerospace_Corporation
Controlled descent
crewed mission
Foundation for future crewed missions
Life support, navigation, and control systems.
Preceded by uncrewed missions
Based_on_Soyuz_design_principles
|
|
gptkbp:missions
|
successful
Automated and manual
5 days, 23 hours, 22 minutes
Demonstrate crewed spaceflight capabilities
Test of crewed spaceflight technology
|
|
gptkbp:operator
|
gptkb:China_National_Space_Administration
|
|
gptkbp:orbitalInclination
|
Low Earth Orbit
90 minutes
42.5 degrees
|
|
gptkbp:powers
|
Solar panels
|
|
gptkbp:renovated
|
Parachute
|
|
gptkbp:respondsTo
|
Yes
|
|
gptkbp:scientificName
|
Yes
|
|
gptkbp:secondaryMission
|
Conducted
|
|
gptkbp:speed
|
7.9 km/s
|
|
gptkbp:successor
|
gptkb:Shenzhou_3
|
|
gptkbp:technology
|
Yes
|
|
gptkbp:weight
|
7,800 kg
|
|
gptkbp:yearEstablished
|
2001-01-15
|