|
gptkbp:instanceOf
|
gptkb:satellite
|
|
gptkbp:application
|
parachute-assisted splashdown
|
|
gptkbp:armament
|
gptkb:Avcoat_ablative_material
|
|
gptkbp:capacity
|
4 astronauts
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:crewSupportDuration
|
up to 21 days active
|
|
gptkbp:designedBy
|
gptkb:Lockheed_Martin_Space_Systems
|
|
gptkbp:designedFor
|
crewed deep space missions
|
|
gptkbp:diameter
|
5.02 meters
|
|
gptkbp:dockedWith
|
gptkb:NASA_Docking_System
|
|
gptkbp:escapeMethod
|
gptkb:Launch_Abort_System
|
|
gptkbp:firstFlight
|
gptkb:Exploration_Flight_Test-1
December 5, 2014
|
|
gptkbp:heatShieldDiameter
|
5 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Orion Crew Module
|
|
gptkbp:launchVehicle
|
gptkb:Space_Launch_System
gptkb:Delta_IV_Heavy
|
|
gptkbp:length
|
5.02 meters
|
|
gptkbp:lifeSupportSystem
|
Regenerative and open-loop
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
|
gptkbp:mass
|
8,500 kg (approximate, uncrewed)
|
|
gptkbp:minimumPressure
|
9 m³
|
|
gptkbp:mission
|
gptkb:Artemis_II
gptkb:Artemis_III
gptkb:Artemis_I
|
|
gptkbp:operator
|
gptkb:NASA
|
|
gptkbp:orbitCapability
|
gptkb:Moon
Earth orbit
|
|
gptkbp:partOf
|
gptkb:Orion_spacecraft
|
|
gptkbp:powerSource
|
solar arrays (via service module)
|
|
gptkbp:primaryMission
|
transport crew beyond low Earth orbit
|
|
gptkbp:reentryCapability
|
Lunar return velocities
|
|
gptkbp:relatedTo
|
gptkb:Artemis_program
gptkb:Constellation_program
|
|
gptkbp:status
|
active
|
|
gptkbp:successor
|
gptkb:satellite
|
|
gptkbp:testFlights
|
gptkb:Exploration_Flight_Test-1
gptkb:Artemis_I
|
|
gptkbp:website
|
https://www.nasa.gov/exploration/systems/orion/index.html
|
|
gptkbp:bfsParent
|
gptkb:Avcoat
gptkb:Crew_Module
gptkb:Artemis_I_mission
|
|
gptkbp:bfsLayer
|
6
|