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gptkbp:instance_of
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gptkb:spacecraft
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|
gptkbp:collaboration
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gptkb:Limited
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|
gptkbp:communication_system
|
Solar panels
S-band
|
|
gptkbp:control_system
|
Inertial navigation system
|
|
gptkbp:crew
|
Not applicable
uncrewed
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|
gptkbp:crew_capacity
|
gptkb:0
|
|
gptkbp:debut
|
gptkb:Yes
|
|
gptkbp:decommissioned
|
gptkb:Yes
|
|
gptkbp:design
|
Based on Russian Soyuz spacecraft
|
|
gptkbp:duration
|
7 days
|
|
gptkbp:first_chinese_spacecraft
|
gptkb:Yes
|
|
gptkbp:first_flight
|
gptkb:Yes
|
|
gptkbp:has_programs
|
Shenzhou program
|
|
gptkbp:height
|
2.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Shenzhou 1
|
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gptkbp:landing_site
|
gptkb:Inner_Mongolia
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|
gptkbp:launch_date
|
November 20, 1999
|
|
gptkbp:launch_mass
|
7,800 kg
|
|
gptkbp:launch_site
|
gptkb:Jiuquan_Satellite_Launch_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Long_March_2_F
|
|
gptkbp:launched
|
gptkb:China_National_Space_Administration
November 20, 1999
|
|
gptkbp:length
|
9.25 m
|
|
gptkbp:mass
|
7,800 kg
|
|
gptkbp:mission_type
|
gptkb:human_spaceflight
|
|
gptkbp:objective
|
Test technologies for future crewed missions
|
|
gptkbp:operator
|
gptkb:China_National_Space_Administration
|
|
gptkbp:orbit_type
|
108
Low Earth Orbit
|
|
gptkbp:orbital_period
|
90 minutes
|
|
gptkbp:payload_capacity
|
Scientific instruments
|
|
gptkbp:recovery_method
|
Parachute landing
|
|
gptkbp:speed
|
November 29, 1999
|
|
gptkbp:success_rate
|
100%
|
|
gptkbp:successor
|
gptkb:Shenzhou_2
|
|
gptkbp:width
|
2.8 m
|
|
gptkbp:bfsParent
|
gptkb:Shenzhou_missions
|
|
gptkbp:bfsLayer
|
6
|