gptkbp:instanceOf
|
crewed spacecraft
|
gptkbp:aircraft
|
2.5 m
2.8 m
three-module design
9.25 m
|
gptkbp:applicationDate
|
April 1, 2002
|
gptkbp:collection
|
telemetry data
|
gptkbp:communicationEquipment
|
radio
|
gptkbp:controls
|
autonomous
|
gptkbp:crew
|
gptkb:Wang_Yaping
gptkb:Yang_Liwei
not applicable
Zhang_Jianqi
|
gptkbp:crewCapacity
|
not applicable
|
gptkbp:crewSize
|
0
1
|
gptkbp:dataTransmission
|
successful
|
gptkbp:environmentalImpact
|
passive
|
gptkbp:firstAwarded
|
new technologies
|
gptkbp:firstFlight
|
Yes
of_the_Shenzhou_series
|
https://www.w3.org/2000/01/rdf-schema#label
|
Shenzhou 3
|
gptkbp:internationalCooperation
|
none
|
gptkbp:landingGear
|
gptkb:Inner_Mongolia
|
gptkbp:launchDate
|
10:00 UTC
March 25, 2002
March 25, 2002, 10:00 UTC
|
gptkbp:launched
|
gptkb:China_National_Space_Administration
successful
LC43/94
|
gptkbp:launchSite
|
gptkb:Jiuquan_Satellite_Launch_Center
7,800 kg
|
gptkbp:launchVehicle
|
Long March 2F
|
gptkbp:manufacturer
|
gptkb:China_Academy_of_Space_Technology
|
gptkbp:mission
|
gptkb:Shenzhou
Low Earth Orbit
modular
uncrewed test flight
decommissioned
Test flight
7,800 kg
|
gptkbp:missions
|
Completed
7 days
ground control
Test life support systems
April 1, 2002
validate spacecraft systems
First crewed test flight of Shenzhou program.
|
gptkbp:navigationEquipment
|
inertial navigation
|
gptkbp:operationalStatus
|
retired
|
gptkbp:orbitalInclination
|
90 minutes
successful
42.5 degrees
|
gptkbp:passenger_traffic
|
1,000 kg
|
gptkbp:payloadCapacity
|
1,000 kg
|
gptkbp:powers
|
solar panels
|
gptkbp:purpose
|
test flight
|
gptkbp:releaseYear
|
April 1, 2002
|
gptkbp:renovated
|
gptkb:Inner_Mongolia
parachute
|
gptkbp:respondsTo
|
successful
|
gptkbp:scientificName
|
various
conducted
|
gptkbp:secondaryMission
|
conducted
|
gptkbp:significance
|
demonstrated technology for future missions
|
gptkbp:speed
|
7.8 km/s
|
gptkbp:succeededBy
|
Yes
|
gptkbp:successor
|
gptkb:Shenzhou_4
|
gptkbp:totalGoals
|
108
|
gptkbp:yearEstablished
|
April 1, 2002
|