|
gptkbp:instanceOf
|
gptkb:satellite
|
|
gptkbp:announced
|
2011
|
|
gptkbp:boosters
|
2
|
|
gptkbp:coreStageEngines
|
gptkb:RS-25
|
|
gptkbp:coreStageFuel
|
liquid hydrogen and liquid oxygen
|
|
gptkbp:costPerLaunch
|
over $2 billion
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:diameter
|
8.4 meters
|
|
gptkbp:firstFlight
|
2022-11-16
|
|
gptkbp:height
|
98 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Space Launch System
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center_LC-39B
|
|
gptkbp:mainContractor
|
gptkb:Aerojet_Rocketdyne
gptkb:Boeing
gptkb:Northrop_Grumman
gptkb:United_Launch_Alliance
|
|
gptkbp:manufacturer
|
gptkb:NASA
|
|
gptkbp:massToTransLunarInjection
|
27,000 kg
|
|
gptkbp:numberOfStages
|
gptkb:Interim_Cryogenic_Propulsion_Stage
|
|
gptkbp:operator
|
gptkb:NASA
|
|
gptkbp:payloadFairingDiameter
|
8.4 meters
|
|
gptkbp:payloadToLEO
|
95,000 kg
|
|
gptkbp:plannedVariants
|
gptkb:Block_2
Block 1
Block 1B
|
|
gptkbp:purpose
|
crew and cargo transport beyond low Earth orbit
|
|
gptkbp:relatedTo
|
gptkb:Artemis_program
|
|
gptkbp:solidBoosterFuel
|
polybutadiene acrylonitrile
|
|
gptkbp:status
|
operational
|
|
gptkbp:successor
|
gptkb:Space_Shuttle
|
|
gptkbp:usedIn
|
gptkb:Artemis_III_(planned)
gptkb:Artemis_II_(planned)
gptkb:Artemis_I
|
|
gptkbp:website
|
https://www.nasa.gov/exploration/systems/sls/index.html
|
|
gptkbp:bfsParent
|
gptkb:international_relations
gptkb:satellite
|
|
gptkbp:bfsLayer
|
4
|