|
gptkbp:instance_of
|
gptkb:Space_Launch_System
|
|
gptkbp:budget
|
$30 billion by 2025
|
|
gptkbp:challenges
|
gptkb:significant
|
|
gptkbp:collaboration
|
yes
|
|
gptkbp:configuration
|
Block 1
|
|
gptkbp:core_stage_diameter
|
8.4 meters
|
|
gptkbp:core_stage_length
|
63 meters
|
|
gptkbp:crew_capacity
|
gptkb:none
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:development
|
gptkb:2011
ongoing
|
|
gptkbp:development_cost
|
$18 billion
|
|
gptkbp:durability
|
no
|
|
gptkbp:engine_type
|
gptkb:RS-25
|
|
gptkbp:environmental_impact
|
studied
|
|
gptkbp:first_flight
|
gptkb:2019
multiple
|
|
gptkbp:fuel_type
|
liquid hydrogen and liquid oxygen
|
|
gptkbp:ground_testing
|
completed
|
|
gptkbp:has_programs
|
gptkb:Artemis_program
|
|
gptkbp:height
|
98 meters
|
|
gptkbp:historical_significance
|
first launch of Artemis program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Space Launch System (SLS) Block 1
|
|
gptkbp:is_a_destination_for
|
gptkb:Moon
|
|
gptkbp:is_tested_for
|
ongoing
|
|
gptkbp:launch_date
|
2024
1 per year
|
|
gptkbp:launch_mass
|
2,900,000 pounds
|
|
gptkbp:launch_platform
|
gptkb:NASA
gptkb:Launch_Complex_39_B
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
two
|
|
gptkbp:launch_window
|
multiple days
|
|
gptkbp:manufacturer
|
gptkb:Boeing
|
|
gptkbp:media_coverage
|
extensive
|
|
gptkbp:mission
|
gptkb:Johnson_Space_Center
gptkb:Artemis_I
deep space exploration
|
|
gptkbp:mission_duration
|
up to 30 days
|
|
gptkbp:number_of_stages
|
gptkb:Interim_Cryogenic_Propulsion_Stage
four RS-25 engines
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:orbital_altitude
|
yes
7.8 km/s
|
|
gptkbp:payload_capacity
|
5 meters
95 metric tons
|
|
gptkbp:propulsion
|
8.4 million pounds
1.8 million pounds per engine
|
|
gptkbp:public_interest
|
high
|
|
gptkbp:recovery_method
|
gptkb:none
|
|
gptkbp:safety_rating
|
high
|
|
gptkbp:scientific_goals
|
gptkb:Mars_exploration
|
|
gptkbp:solid_rocket_booster_diameter
|
3.7 meters
|
|
gptkbp:solid_rocket_booster_length
|
45.2 meters
|
|
gptkbp:upgrades
|
Block 1 B
|
|
gptkbp:upper_stage_fuel
|
liquid hydrogen and liquid oxygen
|
|
gptkbp:upper_stage_thrust
|
60,000 pounds
|
|
gptkbp:bfsParent
|
gptkb:Artemis_I
gptkb:Artemis_missions
|
|
gptkbp:bfsLayer
|
4
|