|
gptkbp:instanceOf
|
gptkb:satellite
|
|
gptkbp:commandModuleProvider
|
gptkb:Lockheed_Martin
|
|
gptkbp:commandModuleType
|
gptkb:Crew_Module
|
|
gptkbp:countryOfOrigin
|
gptkb:European_Union
gptkb:United_States
|
|
gptkbp:designedFor
|
gptkb:Artemis_program
Deep space exploration
|
|
gptkbp:destination
|
gptkb:Mars
gptkb:Moon
|
|
gptkbp:diameter
|
5.02 m
|
|
gptkbp:dockedWith
|
gptkb:NASA_Docking_System
|
|
gptkbp:escapeMethod
|
gptkb:Launch_Abort_System
|
|
gptkbp:firstAppearance
|
gptkb:Artemis_I
|
|
gptkbp:firstFlight
|
2022-11-16
|
|
gptkbp:firstUncrewedFlight
|
gptkb:Exploration_Flight_Test-1
|
|
gptkbp:firstUncrewedFlightDate
|
2014-12-05
|
|
gptkbp:heatShieldMaterial
|
gptkb:Avcoat
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Orion spacecraft
|
|
gptkbp:launchVehicle
|
gptkb:Space_Launch_System
|
|
gptkbp:length
|
5.02 m
|
|
gptkbp:lifeSupportSystem
|
Regenerative
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:mass
|
26,520 kg
|
|
gptkbp:missionDurationCapability
|
21 days active, 6 months docked
|
|
gptkbp:navigationSystem
|
Star trackers and inertial measurement units
|
|
gptkbp:operator
|
gptkb:NASA
gptkb:ESA
|
|
gptkbp:partOf
|
gptkb:Artemis_program
NASA's deep space exploration architecture
|
|
gptkbp:plannedCrewedFlight
|
gptkb:Artemis_II
|
|
gptkbp:plannedCrewedFlightDate
|
2025 (planned)
|
|
gptkbp:powerSource
|
solar panels
|
|
gptkbp:previousName
|
gptkb:Crew_Exploration_Vehicle
|
|
gptkbp:reentryCapability
|
lunar return velocities
|
|
gptkbp:seatingCapacity
|
4
|
|
gptkbp:serviceModuleProvider
|
gptkb:ESA
|
|
gptkbp:serviceModuleType
|
gptkb:European_Service_Module
|
|
gptkbp:status
|
active
|
|
gptkbp:supportsProtocol
|
S-band and Ka-band
|
|
gptkbp:website
|
https://www.nasa.gov/orion/
|
|
gptkbp:bfsParent
|
gptkb:National_Aeronautics_and_Space_Administration
gptkb:satellite
|
|
gptkbp:bfsLayer
|
4
|