|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:affiliatedWith
|
gptkb:Artemis_program
|
|
gptkbp:crewCapacity
|
4 to 6 astronauts
|
|
gptkbp:design
|
Northrop_Grumman,_Aerojet_Rocketdyne
|
|
gptkbp:designedFor
|
gptkb:Artemis_missions
|
|
gptkbp:developer
|
$20 billion
|
|
gptkbp:diameter
|
8.4 meters
|
|
gptkbp:drawings
|
Block 2 core stage
|
|
gptkbp:electronicSystems
|
Complex integration
NASA_engineers_and_contractors
|
|
gptkbp:engineType
|
RS-25
|
|
gptkbp:environmentalImpact
|
Minimized emissions
|
|
gptkbp:filmography
|
gptkb:Orion_spacecraft
|
|
gptkbp:firstAwarded
|
Core stage with four RS-25 engines
|
|
gptkbp:firstFlight
|
2023
2024
Green Run
|
|
gptkbp:fuelType
|
Liquid oxygen and liquid hydrogen
|
|
gptkbp:hasArea
|
gptkb:NASA's_Stennis_Space_Center
|
|
gptkbp:hasFunding
|
NASA_budget
|
|
gptkbp:hasGoals
|
Two solid rocket boosters
|
|
gptkbp:height
|
111 meters
|
|
gptkbp:homeGround
|
gptkb:NASA's_Ground_Systems_Development_and_Operations
|
|
gptkbp:house
|
Interim Cryogenic Propulsion Stage
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SLS Block 2
|
|
gptkbp:integration
|
gptkb:Vehicle_Assembly_Building
|
|
gptkbp:internationalCooperation
|
ESA, JAXA
|
|
gptkbp:launched
|
gptkb:Launch_Complex_39B
6 months
1 to 2 per year
$500 million per launch
2024 to 2025
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launchVehicle
|
Heavy-lift launch vehicle
Block 2 configuration
|
|
gptkbp:manufacturer
|
gptkb:Boeing
|
|
gptkbp:missionCapabilities
|
Deep space exploration
|
|
gptkbp:missions
|
30 days
|
|
gptkbp:missionsConducted
|
Successful crewed lunar landing
|
|
gptkbp:numberOfEpisodes
|
4
|
|
gptkbp:orbitalInclination
|
28,000 km/h
|
|
gptkbp:partOf
|
NASA
|
|
gptkbp:payloadCapacity
|
27 tons
95 tons
|
|
gptkbp:primaryMission
|
Lunar exploration
Mars_exploration
|
|
gptkbp:productionCompany
|
2011
|
|
gptkbp:project
|
gptkb:NASA_Marshall_Space_Flight_Center
2024
2020s
$30 billion by 2030
|
|
gptkbp:propulsion
|
2,000,000 pounds
|
|
gptkbp:publicAccess
|
High
|
|
gptkbp:reliability
|
Not reusable
|
|
gptkbp:safetyFeatures
|
Redundant systems
|
|
gptkbp:secondaryMission
|
Artemis II, Artemis III
|
|
gptkbp:successor
|
gptkb:SLS_Block_1
|
|
gptkbp:technology
|
Development delays
|