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gptkbp:instanceOf
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gptkb:satellite
|
|
gptkbp:abortSystem
|
gptkb:SuperDraco_engines
|
|
gptkbp:alsoKnownAs
|
gptkb:Crew_Dragon
|
|
gptkbp:armament
|
gptkb:PICA-X
|
|
gptkbp:autonomousDocking
|
yes
|
|
gptkbp:builtBy
|
gptkb:SpaceX
|
|
gptkbp:canBeOperatedAutonomously
|
yes
|
|
gptkbp:canBeOperatedManually
|
yes
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:designedFor
|
gptkb:NASA_Commercial_Crew_Program
|
|
gptkbp:diameter
|
4.0 m
|
|
gptkbp:dockedWith
|
gptkb:NASA_Docking_System
|
|
gptkbp:escapeMethod
|
integrated launch escape system
|
|
gptkbp:firstCrewedMission
|
gptkb:Demo-2
|
|
gptkbp:firstFlight
|
30 May 2020
|
|
gptkbp:firstOperationalMission
|
gptkb:Crew-1
|
|
gptkbp:hasRestrooms
|
yes
|
|
gptkbp:hasTouchscreenControls
|
yes
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Dragon 2 (Crew variant)
|
|
gptkbp:launchMass
|
12,055 kg
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center_LC-39A
|
|
gptkbp:launchVehicle
|
gptkb:Falcon_9
|
|
gptkbp:length
|
8.1 m
|
|
gptkbp:lifeSupportSystem
|
yes
|
|
gptkbp:majorCity
|
gptkb:International_Space_Station
|
|
gptkbp:manufacturer
|
gptkb:SpaceX
|
|
gptkbp:minimumPressure
|
9.3 m³
|
|
gptkbp:missions
|
gptkb:Axiom_Mission_2
gptkb:Axiom_Mission_1
gptkb:Crew-1
gptkb:Crew-2
gptkb:Crew-3
gptkb:Crew-4
gptkb:Crew-5
gptkb:Crew-6
gptkb:Crew-7
gptkb:Crew-8
gptkb:Demo-2
gptkb:Inspiration4
gptkb:Polaris_Dawn
|
|
gptkbp:missionType
|
crewed spaceflight
|
|
gptkbp:operator
|
gptkb:SpaceX
|
|
gptkbp:partOf
|
gptkb:Commercial_Crew_Program
|
|
gptkbp:powerSource
|
solar panels
|
|
gptkbp:propulsion
|
gptkb:Draco_thrusters
|
|
gptkbp:reusable
|
true
|
|
gptkbp:seatingCapacity
|
7
|
|
gptkbp:status
|
active
|
|
gptkbp:successor
|
gptkb:Dragon_1
|
|
gptkbp:unpressurizedTrunkVolume
|
37 m³
|
|
gptkbp:bfsParent
|
gptkb:Dragon_2_(Cargo_variant)
|
|
gptkbp:bfsLayer
|
8
|