|
gptkbp:instanceOf
|
gptkb:Soviet_space_program
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:designedFor
|
Mars missions
long-duration missions
asteroid missions
Moon missions
|
|
gptkbp:developedBy
|
gptkb:Lockheed_Martin
|
|
gptkbp:diameter
|
5.02 m
|
|
gptkbp:escapeMethod
|
gptkb:Launch_Abort_System
|
|
gptkbp:firstCrewedMission
|
gptkb:Artemis_II_(planned)
|
|
gptkbp:firstFlight
|
December 5, 2014
|
|
gptkbp:firstUncrewedFlight
|
gptkb:Exploration_Flight_Test-1
|
|
gptkbp:heatShieldMaterial
|
gptkb:Avcoat
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Orion spacecraft program
|
|
gptkbp:initialName
|
gptkb:Crew_Exploration_Vehicle
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launchVehicle
|
gptkb:Space_Launch_System
|
|
gptkbp:length
|
5.02 m (crew module)
|
|
gptkbp:lifeSupportSystem
|
regenerative
|
|
gptkbp:mainContractor
|
gptkb:Lockheed_Martin
|
|
gptkbp:mass
|
~26,000 kg (with service module)
|
|
gptkbp:operatedBy
|
gptkb:NASA
|
|
gptkbp:partOf
|
gptkb:Artemis_program
|
|
gptkbp:powerSource
|
solar arrays
|
|
gptkbp:predecessor
|
gptkb:Apollo_program
|
|
gptkbp:purpose
|
crewed deep space exploration
|
|
gptkbp:reentryCapability
|
high-speed lunar return
|
|
gptkbp:relatedTo
|
gptkb:Artemis_II
gptkb:Exploration_Flight_Test-1
gptkb:Artemis_III
gptkb:Artemis_I
gptkb:Ascent_Abort-2
|
|
gptkbp:seatingCapacity
|
4
|
|
gptkbp:serviceModuleBuiltBy
|
gptkb:Airbus_Defence_and_Space
|
|
gptkbp:serviceModuleProvider
|
gptkb:European_Space_Agency
|
|
gptkbp:status
|
active
|
|
gptkbp:supportsProtocol
|
S-band, Ka-band
|
|
gptkbp:website
|
https://www.nasa.gov/exploration/systems/orion/index.html
|
|
gptkbp:bfsParent
|
gptkb:Howard_Hu
|
|
gptkbp:bfsLayer
|
6
|