Shenzhou 4

GPTKB entity

Properties (51)
Predicate Object
gptkbp:instanceOf crewed spacecraft
gptkbp:caseOutcome successful
gptkbp:crew not applicable
gptkbp:crewSize 0
gptkbp:design based_on_the_Russian_Soyuz_spacecraft
gptkbp:duration 5 days
gptkbp:firstFlight gptkb:Shenzhou_program
gptkbp:followedBy gptkb:Shenzhou_5
gptkbp:hasArea propulsion systems
communication systems
life support systems
spacecraft systems
reentry technology
thermal control systems
autonomous flight capabilities
recovery systems
navigation_systems
https://www.w3.org/2000/01/rdf-schema#label Shenzhou 4
gptkbp:internationalCooperation none
gptkbp:landingGear Siberia,_Russia
gptkbp:launchDate December 30, 2002
gptkbp:launched successful
gptkbp:launchSite gptkb:Jiuquan_Satellite_Launch_Center
approximately 7,800 kg
gptkbp:launchVehicle Long March 2F
gptkbp:mission manned spaceflight
orbital module
reentry capsule
service module
gptkbp:missions 5 days, 22 hours, 12 minutes
gptkbp:operationalStatus retired
gptkbp:operator gptkb:China_National_Space_Administration
gptkbp:orbitalInclination approximately 90 minutes
42.0 degrees
approximately 343 km
gptkbp:passenger_traffic propulsion systems
autonomous systems
communication equipment
scientific instruments
life support systems
navigation equipment
approximately 2,500 kg
thermal control systems
recovery systems
technology demonstration equipment
gptkbp:purpose test technologies for future crewed missions
gptkbp:respondsTo January 5, 2003
gptkbp:significance paved_the_way_for_Shenzhou_5
important_step_in_China's_human_spaceflight_program
gptkbp:successor gptkb:Shenzhou_5
gptkbp:weight approximately 7,800 kg