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
|