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gptkbp:instanceOf
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gptkb:satellite
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gptkbp:application
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parachute-assisted splashdown
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gptkbp:armament
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gptkb:Avcoat
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gptkbp:avionics
|
triple-redundant flight computers
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|
gptkbp:communication
|
S-band and Ka-band radio
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gptkbp:compatibleWith
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gptkb:European_Service_Module
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gptkbp:countryOfOrigin
|
gptkb:United_States
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gptkbp:designedFor
|
Mars missions
lunar missions
deep space missions
autonomously operate
be reused up to 10 times
dock with Gateway lunar outpost
operate up to 21 days in space without docking
support long-duration missions
support up to 6 months docked to a space station
withstand micrometeoroid impacts
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gptkbp:developedBy
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gptkb:NASA
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gptkbp:diameter
|
5.02 meters
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gptkbp:emergencySystem
|
launch abort system
|
|
gptkbp:escapeMethod
|
gptkb:Launch_Abort_System
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gptkbp:firstFlight
|
gptkb:Exploration_Flight_Test-1
December 5, 2014
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gptkbp:hatch
|
side and docking hatches
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Orion crew module
|
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gptkbp:launchVehicle
|
gptkb:Space_Launch_System
gptkb:Delta_IV_Heavy
|
|
gptkbp:length
|
5.02 meters
|
|
gptkbp:lifeSupportSystem
|
gptkb:Environmental_Control_and_Life_Support_System
|
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gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
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gptkbp:mass
|
8,500 kg
|
|
gptkbp:minimumPressure
|
9 cubic meters
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|
gptkbp:navigationSystem
|
star trackers and inertial measurement units
|
|
gptkbp:numberOfWindows
|
6
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gptkbp:partOf
|
gptkb:Orion_spacecraft
|
|
gptkbp:powerSource
|
solar panels
|
|
gptkbp:primaryUser
|
gptkb:NASA
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|
gptkbp:radiationProtection
|
enhanced shielding
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|
gptkbp:reentryCapability
|
lunar return velocities
|
|
gptkbp:seatingCapacity
|
4
|
|
gptkbp:secondaryUser
|
gptkb:ESA_(European_Space_Agency)
|
|
gptkbp:shape
|
blunt-body capsule
|
|
gptkbp:status
|
in service
|
|
gptkbp:thermalProtection
|
ablative heat shield
|
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gptkbp:usedIn
|
gptkb:Artemis_III_(planned)
gptkb:Artemis_II_(planned)
gptkb:Artemis_I
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gptkbp:bfsParent
|
gptkb:Orion_Launch_Abort_System
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gptkbp:bfsLayer
|
7
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