|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:crew
|
Ongoing
|
|
gptkbp:crewCapacity
|
4 astronauts
|
|
gptkbp:design
|
10 years
|
|
gptkbp:developer
|
$20 billion
|
|
gptkbp:diameter
|
8.4 meters
|
|
gptkbp:drawings
|
4 engines
|
|
gptkbp:electronicSystems
|
High
NASA_engineers
|
|
gptkbp:engine
|
4
|
|
gptkbp:engineType
|
RS-25
|
|
gptkbp:environmentalImpact
|
Completed
|
|
gptkbp:filmography
|
Lunar landers
|
|
gptkbp:financialPerformance
|
Lunar exploration
|
|
gptkbp:firstFlight
|
2028
1 planned
|
|
gptkbp:firstHomePort
|
8.4 million pounds
|
|
gptkbp:fuelType
|
Liquid hydrogen and liquid oxygen
|
|
gptkbp:hasArea
|
NASA_facilities
|
|
gptkbp:hasFunding
|
Yes
|
|
gptkbp:hasGoals
|
2
|
|
gptkbp:height
|
98 meters
|
|
gptkbp:homeGround
|
Custom-built
|
|
gptkbp:house
|
ICPS
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SLS Block 8
|
|
gptkbp:integration
|
6 months
|
|
gptkbp:internationalCooperation
|
Yes
|
|
gptkbp:launched
|
gptkb:Launch_Complex_39B
1 year
$2 billion
Open-ended
1 per year
NASA_ground_crew
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launchVehicle
|
Heavy-lift launch vehicle
SLS
|
|
gptkbp:manufacturer
|
NASA
|
|
gptkbp:mission
|
gptkb:Artemis_program
Lunar missions
|
|
gptkbp:missions
|
gptkb:Johnson_Space_Center
30 days
Sustainable lunar presence
|
|
gptkbp:orbitalInclination
|
Yes
7.8 km/s
|
|
gptkbp:partOf
|
NASA
|
|
gptkbp:payloadCapacity
|
27 tons
95 tons
|
|
gptkbp:productionCompany
|
In development
|
|
gptkbp:project
|
NASA
2028
$2 billion per launch
|
|
gptkbp:propulsion
|
2,000,000 pounds
|
|
gptkbp:publicAccess
|
High
|
|
gptkbp:releaseFormat
|
39B
|
|
gptkbp:reliability
|
Not reusable
|
|
gptkbp:renovated
|
Not applicable
|
|
gptkbp:safety
|
High
|
|
gptkbp:safetyFeatures
|
Ongoing
|
|
gptkbp:secondaryMission
|
Mars_missions_planned
|
|
gptkbp:sustainabilityPractices
|
Incorporated
|
|
gptkbp:targets
|
2028
|
|
gptkbp:technology
|
Yes
|