|
gptkbp:instanceOf
|
gptkb:satellite
|
|
gptkbp:avionicsSupplier
|
gptkb:Honeywell
|
|
gptkbp:backupMission
|
International Space Station crew transport (not implemented)
|
|
gptkbp:communication
|
S-band and Ka-band
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:crewModuleVolume
|
9 m³
|
|
gptkbp:designedBy
|
gptkb:NASA
|
|
gptkbp:designedFor
|
lunar missions
asteroid missions
beyond low Earth orbit missions
|
|
gptkbp:diameter
|
5.02 m
|
|
gptkbp:dockedWith
|
gptkb:NASA_Docking_System
|
|
gptkbp:engine
|
gptkb:Aerojet_Rocketdyne_AJ10
|
|
gptkbp:escapeMethod
|
gptkb:Launch_Abort_System
|
|
gptkbp:firstCrewedMission
|
gptkb:Artemis_II_(planned)
|
|
gptkbp:firstFlight
|
gptkb:Exploration_Flight_Test-1
December 5, 2014
|
|
gptkbp:firstServiceModuleFlight
|
gptkb:Artemis_I
|
|
gptkbp:firstServiceModuleProvider
|
gptkb:European_Space_Agency
|
|
gptkbp:firstUncrewedFlight
|
gptkb:Exploration_Flight_Test-1
|
|
gptkbp:guidanceSystem
|
gptkb:Honeywell_Inertial_Measurement_Unit
|
|
gptkbp:heatShieldDiameter
|
5 m
|
|
gptkbp:heatShieldMaterial
|
gptkb:Avcoat
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Orion MPCV
|
|
gptkbp:intendedUse
|
gptkb:Artemis_program
gptkb:Deep_Space_Gateway
Mars missions
|
|
gptkbp:launchVehicle
|
gptkb:Space_Launch_System
gptkb:Delta_IV_Heavy
|
|
gptkbp:length
|
5.02 m
|
|
gptkbp:lifeSupportDuration
|
21 days (active crewed mission)
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:mass
|
25,848 kg
|
|
gptkbp:maximumOrbitDuration
|
6 months (docked to Gateway)
|
|
gptkbp:missionType
|
crewed spaceflight
|
|
gptkbp:namedAfter
|
gptkb:Orion_constellation
|
|
gptkbp:navigationSystem
|
star trackers and inertial measurement units
|
|
gptkbp:operator
|
gptkb:NASA
|
|
gptkbp:partOf
|
gptkb:NASA_Artemis_program
|
|
gptkbp:powerSource
|
solar panels
|
|
gptkbp:previousName
|
gptkb:Orion_Crew_Exploration_Vehicle
|
|
gptkbp:primaryMission
|
transport astronauts beyond low Earth orbit
|
|
gptkbp:propulsion
|
monomethylhydrazine and nitrogen tetroxide
|
|
gptkbp:reentryCapability
|
high-velocity reentry
|
|
gptkbp:seatingCapacity
|
4
|
|
gptkbp:serviceModuleProvider
|
gptkb:Airbus_Defence_and_Space
|
|
gptkbp:serviceModuleType
|
gptkb:European_Service_Module
|
|
gptkbp:serviceModuleVolume
|
19.8 m³
|
|
gptkbp:shape
|
conical
|
|
gptkbp:status
|
active
|
|
gptkbp:thermalProtection
|
gptkb:Avcoat_ablative_material
|
|
gptkbp:website
|
https://www.nasa.gov/exploration/systems/orion/index.html
|
|
gptkbp:bfsParent
|
gptkb:Exploration_Flight_Test-1
gptkb:Artemis_II_(assigned)
gptkb:Avcoat
gptkb:Orion_EFT-1
gptkb:Artemis_II_(as_commander)
|
|
gptkbp:bfsLayer
|
6
|