|
gptkbp:instanceOf
|
rocket stage
|
|
gptkbp:assemblyLocation
|
gptkb:NASA_Michoud_Assembly_Facility
|
|
gptkbp:built
|
2021
|
|
gptkbp:communicationEquipment
|
secure telemetry
|
|
gptkbp:controls
|
digital flight control
|
|
gptkbp:coolingSystem
|
active cooling
|
|
gptkbp:designedBy
|
NASA
|
|
gptkbp:diameter
|
8.4 meters
|
|
gptkbp:electronicSystems
|
high thrust-to-weight ratio
redundant power systems
|
|
gptkbp:engine
|
dampers
|
|
gptkbp:engineType
|
RS-25
|
|
gptkbp:environmentalImpact
|
life support systems
|
|
gptkbp:firstFlight
|
Artemis I
|
|
gptkbp:fuelCapacity
|
1,500,000 liters
|
|
gptkbp:futurePlans
|
Block 1B and Block 2
|
|
gptkbp:gameFeatures
|
liquid hydrogen and liquid oxygen
|
|
gptkbp:hasArea
|
gptkb:NASA_Stennis_Space_Center
static fire tests
|
|
gptkbp:height
|
65 meters
|
|
gptkbp:historicalSignificance
|
part_of_Artemis_program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SLS Core Stage
|
|
gptkbp:integration
|
several months
with_the_Orion_spacecraft
|
|
gptkbp:internationalCooperation
|
with_ESA_and_other_agencies
|
|
gptkbp:launched
|
varies by mission
approximately once a year
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center
Block 1
2,900,000 pounds
|
|
gptkbp:mission
|
deep space exploration
|
|
gptkbp:missions
|
return humans to the Moon
|
|
gptkbp:numberOfEpisodes
|
four RS-25 engines
|
|
gptkbp:partOf
|
gptkb:Space_Launch_System
|
|
gptkbp:payloadCapacity
|
95 metric tons
27 metric tons
|
|
gptkbp:producedBy
|
NASA_and_contractors
|
|
gptkbp:productionCompany
|
2011
|
|
gptkbp:project
|
$20 billion
|
|
gptkbp:propulsion
|
2,000,000 pounds
|
|
gptkbp:publicAccess
|
high
|
|
gptkbp:reliability
|
not_reusable
|
|
gptkbp:safetyFeatures
|
redundant systems
|
|
gptkbp:secondaryMission
|
Mars_exploration_missions
|
|
gptkbp:sustainability
|
recycling materials
|
|
gptkbp:technology
|
advanced propulsion systems
|
|
gptkbp:transportation
|
barge
|
|
gptkbp:usedFor
|
launching crewed missions
|