|
gptkbp:instanceOf
|
gptkb:satellite
|
|
gptkbp:alternativeName
|
CZ-2F
Chang Zheng 2F
LM-2F
|
|
gptkbp:boosterDiameter
|
2.25 m
|
|
gptkbp:boosterLength
|
15.33 m
|
|
gptkbp:boosterPropellant
|
UDMH/N2O4
|
|
gptkbp:boosters
|
4
|
|
gptkbp:coreRadius
|
3.35 m
|
|
gptkbp:countryOfOrigin
|
gptkb:China
|
|
gptkbp:derivedFrom
|
gptkb:Long_March_2E
|
|
gptkbp:diameter
|
3.35 m
|
|
gptkbp:family
|
gptkb:Long_March_rocket_family
|
|
gptkbp:firstFlight
|
1999-11-19
|
|
gptkbp:guidanceSystem
|
inertial
|
|
gptkbp:hasModel
|
YF
|
|
gptkbp:height
|
62 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Long March 2F rocket
|
|
gptkbp:launchSite
|
gptkb:Jiuquan_Satellite_Launch_Center
|
|
gptkbp:length
|
62 m
|
|
gptkbp:manufacturer
|
gptkb:China_Academy_of_Launch_Vehicle_Technology
|
|
gptkbp:mass
|
479,800 kg
|
|
gptkbp:notableFeature
|
launch escape system
human-rated
|
|
gptkbp:notableMission
|
gptkb:Shenzhou_5
gptkb:Shenzhou_14
gptkb:Shenzhou_9
gptkb:Shenzhou_6
gptkb:Shenzhou_10
gptkb:Shenzhou_13
gptkb:Shenzhou_15
gptkb:Shenzhou_11
gptkb:Shenzhou_16
gptkb:Shenzhou_17
gptkb:Shenzhou_18
gptkb:Shenzhou_8
gptkb:Shenzhou_7
gptkb:Shenzhou_12
gptkb:Tiangong-1
gptkb:Tiangong-2
|
|
gptkbp:numberOfStages
|
2
|
|
gptkbp:operator
|
gptkb:China_National_Space_Administration
|
|
gptkbp:payloadToLEO
|
8,400 kg
|
|
gptkbp:propellantFirstStage
|
UDMH/N2O4
|
|
gptkbp:propulsion
|
UDMH/N2O4
|
|
gptkbp:secondStagePropellant
|
UDMH/N2O4
|
|
gptkbp:status
|
active
|
|
gptkbp:usedFor
|
gptkb:Shenzhou_missions
gptkb:Tiangong_missions
crewed spaceflight
|
|
gptkbp:bfsParent
|
gptkb:Project_921
|
|
gptkbp:bfsLayer
|
8
|