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gptkbp:instanceOf
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gptkb:spacecraft
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gptkbp:affiliatedWith
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gptkb:Artemis_program
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gptkbp:controls
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digital fly-by-wire
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gptkbp:crewCapacity
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up to 4 astronauts
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gptkbp:designedFor
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gptkb:Artemis_missions
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gptkbp:developer
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gptkb:NASA_Marshall_Space_Flight_Center
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gptkbp:drawings
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four engines
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gptkbp:engineType
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RS-25
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gptkbp:firstAwarded
|
core stage with four RS-25 engines
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gptkbp:firstFlight
|
Artemis I
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gptkbp:fuelType
|
liquid hydrogen and liquid oxygen
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|
gptkbp:futurePlans
|
Block 2 configuration planned
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gptkbp:hasArea
|
B-2 Test Stand
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gptkbp:hasGoals
|
two
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gptkbp:height
|
98 meters
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|
gptkbp:historicalSignificance
|
part of returning humans to the Moon
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gptkbp:homeGround
|
custom-built
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gptkbp:house
|
ICPS (Interim Cryogenic Propulsion Stage)
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|
https://www.w3.org/2000/01/rdf-schema#label
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SLS Block 9
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gptkbp:integration
|
approximately 12 months
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|
gptkbp:internationalCooperation
|
with_ESA_and_JAXA
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gptkbp:launched
|
gptkb:Launch_Complex_39B
NASA astronauts
specific to mission
once every two years
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center
3,000,000 kg
|
|
gptkbp:manufacturer
|
gptkb:Boeing
|
|
gptkbp:mission
|
crewed and uncrewed missions
|
|
gptkbp:missions
|
gptkb:Johnson_Space_Center
up to 30 days
|
|
gptkbp:notableFeature
|
2024
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|
gptkbp:orbitalInclination
|
Lunar orbit
up to 28,000 km/h
|
|
gptkbp:partOf
|
NASA
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|
gptkbp:passenger_traffic
|
5 meters in diameter
|
|
gptkbp:payloadCapacity
|
up to 130 metric tons
|
|
gptkbp:productionCompany
|
2011
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gptkbp:project
|
$2 billion per launch
|
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gptkbp:publicAccess
|
educational outreach programs
|
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gptkbp:reliability
|
not_reusable
|
|
gptkbp:safetyFeatures
|
multiple redundant systems
|
|
gptkbp:setting
|
Block 1B
|
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gptkbp:successor
|
Space Shuttle
|
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gptkbp:sustainability
|
designed for long-term lunar exploration
|
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gptkbp:targets
|
gptkb:Moon
|