|
gptkbp:instanceOf
|
rocket
|
|
gptkbp:averageRainfall
|
$30 billion by 2025
|
|
gptkbp:collaborations
|
gptkb:JAXA
gptkb:ESA
CSA
|
|
gptkbp:community_engagement
|
high
|
|
gptkbp:construction_cost
|
$18 billion
|
|
gptkbp:crew_size
|
up to 4 astronauts
|
|
gptkbp:design
|
gptkb:Lockheed_Martin
gptkb:Northrop_Grumman
gptkb:Boeing
15 years
Aerojet Rocketdyne
|
|
gptkbp:diameter
|
8.4 meters
|
|
gptkbp:engineType
|
RS-25
|
|
gptkbp:environmental_impact
|
minimized emissions
|
|
gptkbp:first_held
|
initial configuration
|
|
gptkbp:firstFlight
|
2021
multiple
|
|
gptkbp:future_plans
|
ongoing
|
|
gptkbp:height
|
98 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Space Launch Systems
|
|
gptkbp:inspiration
|
gptkb:Saturn_V
Space Shuttle
Ares I
|
|
gptkbp:launchDate
|
1-2 launches per year
|
|
gptkbp:launched
|
2
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launchVehicle
|
heavy-lift
NASA's_primary_launch_vehicle
|
|
gptkbp:manufacturer
|
NASA
|
|
gptkbp:maxTakeoffWeight
|
2,600,000 pounds
|
|
gptkbp:media_coverage
|
extensive
|
|
gptkbp:mission
|
deep space exploration
|
|
gptkbp:missions
|
gptkb:Johnson_Space_Center
Artemis II
|
|
gptkbp:nesting
|
enhanced configuration
|
|
gptkbp:number_of_stages
|
2
liquid-fueled
|
|
gptkbp:orbitalInclination
|
Lunar orbit
|
|
gptkbp:passenger_traffic
|
95 metric tons to low Earth orbit
|
|
gptkbp:produces
|
2011
|
|
gptkbp:purpose
|
crewed and uncrewed missions
|
|
gptkbp:relatedPatent
|
gptkb:Artemis_program
|
|
gptkbp:reliability
|
partially reusable
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:secondary_mission
|
Artemis I
|
|
gptkbp:technology
|
advanced propulsion systems
|