|
gptkbp:instanceOf
|
rocket
|
|
gptkbp:barrelLength
|
45.2 meters
|
|
gptkbp:crew
|
NASA Astronaut Corps
|
|
gptkbp:crewCapacity
|
up to 4 astronauts
|
|
gptkbp:design
|
gptkb:Boeing
15 years
|
|
gptkbp:developer
|
estimated $18 billion
|
|
gptkbp:drawings
|
four RS-25 engines
|
|
gptkbp:electronicSystems
|
NASA_engineers_and_contractors
|
|
gptkbp:engineType
|
RS-25
|
|
gptkbp:environmentalImpact
|
assessed
|
|
gptkbp:firstFlight
|
2021
Green Run
|
|
gptkbp:firstGeneration
|
conducted after each mission
|
|
gptkbp:fuelType
|
liquid hydrogen and liquid oxygen
|
|
gptkbp:future_plans
|
gptkb:Artemis_program
|
|
gptkbp:hasArea
|
gptkb:NASA_Stennis_Space_Center
|
|
gptkbp:hasFunding
|
government funded
|
|
gptkbp:hasGoals
|
two
|
|
gptkbp:height
|
98 meters
|
|
gptkbp:historicalSignificance
|
important for space exploration
|
|
gptkbp:homeGround
|
custom-built
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SLS (Space Launch System)
|
|
gptkbp:inspiration
|
gptkb:Apollo_program
|
|
gptkbp:integration
|
gptkb:NASA_Michoud_Assembly_Facility
|
|
gptkbp:internationalCooperation
|
ESA, JAXA
|
|
gptkbp:ISO639-3
|
future configuration
|
|
gptkbp:launched
|
gptkb:NASA_Launch_Services_Program
LC-39B
several months
varies by mission
estimated $2 billion per launch
once every 2-3 years
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:manufacturer
|
NASA
|
|
gptkbp:mediaCoverage
|
extensive
|
|
gptkbp:mission
|
crewed and uncrewed missions
|
|
gptkbp:missions
|
gptkb:Johnson_Space_Center
varies by mission
|
|
gptkbp:nesting
|
initial configuration
|
|
gptkbp:notableEvent
|
2011
|
|
gptkbp:orbitalInclination
|
28,000 km/h
performed_by_Orion
|
|
gptkbp:partnerships
|
commercial space companies
|
|
gptkbp:payloadCapacity
|
up to 130 metric tons
|
|
gptkbp:project
|
NASA_program_management
|
|
gptkbp:publicAccess
|
high
held for educational purposes
|
|
gptkbp:purpose
|
deep space exploration
|
|
gptkbp:reliability
|
high
not_reusable
|
|
gptkbp:rotorDiameter
|
3.7 meters
8.4 meters
|
|
gptkbp:safety
|
high
|
|
gptkbp:secondaryMission
|
Artemis I
Artemis II, Artemis III
|
|
gptkbp:sequel
|
enhanced configuration
|
|
gptkbp:successor
|
gptkb:Orion_spacecraft
|
|
gptkbp:sustainability
|
considered in design
|
|
gptkbp:technology
|
overcome during development
|