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gptkbp:instance_of
|
gptkb:Space_Launch_System
|
|
gptkbp:collaboration
|
gptkb:Canadian_Space_Agency
gptkb:European_Space_Agency
gptkb:Japanese_Aerospace_Exploration_Agency
|
|
gptkbp:configuration
|
Block 1
Block 2
Block 1 B
|
|
gptkbp:crew_capacity
|
4-6 astronauts
|
|
gptkbp:design
|
gptkb:Aerojet_Rocketdyne
gptkb:Lockheed_Martin
gptkb:Northrop_Grumman
gptkb:Boeing
|
|
gptkbp:development
|
gptkb:2011
|
|
gptkbp:development_cost
|
$18 billion
|
|
gptkbp:durability
|
no
|
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gptkbp:engine_type
|
gptkb:RS-25
|
|
gptkbp:first_flight
|
gptkb:Artemis_II
gptkb:2019
gptkb:2020
successful
Green Run
|
|
gptkbp:has_programs
|
gptkb:Artemis_program
|
|
gptkbp:height
|
98 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
U. S. Space Launch System
|
|
gptkbp:infrastructure
|
gptkb:Vehicle_Assembly_Building
gptkb:Control_Panel
Mobile Launcher
Crawlway
|
|
gptkbp:is_a_destination_for
|
gptkb:Moon
gptkb:Mars
|
|
gptkbp:launch_date
|
1-2 missions per year
|
|
gptkbp:launch_platform
|
gptkb:Launch_Complex_39_B
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
two
|
|
gptkbp:launch_window
|
varies by mission
|
|
gptkbp:manufacturer
|
gptkb:NASA
|
|
gptkbp:mission
|
gptkb:Johnson_Space_Center
gptkb:Artemis_I
|
|
gptkbp:mission_duration
|
varies by mission
|
|
gptkbp:number_of_stages
|
four RS-25 engines
|
|
gptkbp:orbital_altitude
|
7.8 km/s
|
|
gptkbp:payload_capacity
|
95 metric tons
|
|
gptkbp:payload_capacity_translunar_injection
|
27 metric tons
|
|
gptkbp:projected_operational_date
|
2024
|
|
gptkbp:purpose
|
deep space exploration
|
|
gptkbp:safety_features
|
redundant systems
abort system
|
|
gptkbp:solid_rocket_booster_diameter
|
3.7 meters
|
|
gptkbp:solid_rocket_booster_length
|
45.2 meters
|
|
gptkbp:successor
|
gptkb:Space_Shuttle
|
|
gptkbp:total_launch_weight
|
2.9 million kg
|
|
gptkbp:bfsParent
|
gptkb:Space_Launch_Complex_20
|
|
gptkbp:bfsLayer
|
5
|