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gptkbp:instanceOf
|
gptkb:satellite
|
|
gptkbp:boosters
|
4
|
|
gptkbp:boostersDiameter
|
3.35 m
|
|
gptkbp:boostersLength
|
26.28 m
|
|
gptkbp:boostersPropellant
|
kerosene
liquid oxygen
|
|
gptkbp:countryOfOrigin
|
gptkb:China
|
|
gptkbp:diameter
|
5 m
|
|
gptkbp:enginesBoosters
|
gptkb:YF-100
|
|
gptkbp:enginesFirstStage
|
gptkb:YF-77
|
|
gptkbp:enginesSecondStage
|
YF-75D
|
|
gptkbp:failedLaunches
|
1
|
|
gptkbp:family
|
gptkb:Long_March
|
|
gptkbp:firstFlight
|
2016-11-03
|
|
gptkbp:height
|
57 m
|
|
gptkbp:launchSite
|
gptkb:Wenchang_Space_Launch_Site
|
|
gptkbp:manufacturer
|
gptkb:China_Academy_of_Launch_Vehicle_Technology
|
|
gptkbp:mass
|
867,000 kg
|
|
gptkbp:nickname
|
Pang-Wu
|
|
gptkbp:notableMission
|
gptkb:Tianwen-1_Mars_mission
Chang'e 5 lunar sample return mission
Tianhe space station module
|
|
gptkbp:numberOfLaunches
|
10
9
|
|
gptkbp:numberOfStages
|
2
|
|
gptkbp:operator
|
gptkb:China_National_Space_Administration
|
|
gptkbp:payloadToGTO
|
14,000 kg
|
|
gptkbp:payloadToLEO
|
25,000 kg
|
|
gptkbp:propulsion
|
kerosene
liquid oxygen
liquid hydrogen
|
|
gptkbp:secondStageDiameter
|
5 m
|
|
gptkbp:secondStageLength
|
12.0 m
|
|
gptkbp:secondStagePropellant
|
liquid oxygen
liquid hydrogen
|
|
gptkbp:status
|
active
|
|
gptkbp:usedFor
|
Mars missions
lunar missions
launching satellites
launching space station modules
|
|
gptkbp:variant
|
CZ-5B
CZ-5E
|
|
gptkbp:website
|
http://www.spacechina.com
|
|
gptkbp:bfsParent
|
gptkb:China_Academy_of_Launch_Vehicle_Technology
|
|
gptkbp:bfsLayer
|
7
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CZ-5 (Long March 5)
|