|
gptkbp:instance_of
|
gptkb:Space_Launch_System
|
|
gptkbp:collaboration
|
ESA, JAXA
|
|
gptkbp:community_engagement
|
NASA Social Media Campaigns
|
|
gptkbp:configuration
|
Block 1
|
|
gptkbp:control_system
|
Fly-by-wire
|
|
gptkbp:core_stage_diameter
|
8.4 meters
|
|
gptkbp:core_stage_length
|
63 meters
|
|
gptkbp:core_stage_thrust
|
2 million pounds
|
|
gptkbp:crew
|
NASA Astronaut Training
|
|
gptkbp:crew_capacity
|
gptkb:0
|
|
gptkbp:design
|
15 years
|
|
gptkbp:development_cost
|
$18 billion
|
|
gptkbp:durability
|
No
|
|
gptkbp:engine
|
gptkb:RS-25
|
|
gptkbp:environmental_impact
|
NASA Environmental Assessments
|
|
gptkbp:facilities
|
gptkb:NASA_Stennis_Space_Center
|
|
gptkbp:first_flight
|
gptkb:2019
|
|
gptkbp:fuel_type
|
Liquid Oxygen and Liquid Hydrogen
|
|
gptkbp:guidance_system
|
gptkb:Inertial_Navigation_System
|
|
gptkbp:has_programs
|
gptkb:Artemis_program
|
|
gptkbp:healthcare
|
Telemetry and Tracking
|
|
gptkbp:height
|
98 meters
|
|
gptkbp:historical_significance
|
First launch of Artemis program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
NASA SLS Block 1
|
|
gptkbp:icpsdiameter
|
4.0 meters
|
|
gptkbp:icpslength
|
5.4 meters
|
|
gptkbp:icpsthrust
|
50,000 pounds
|
|
gptkbp:is_integrated_with
|
gptkb:Vehicle_Assembly_Building
|
|
gptkbp:launch_date
|
1 per year
|
|
gptkbp:launch_mass
|
2,900,000 pounds
|
|
gptkbp:launch_platform
|
gptkb:NASA_Launch_Control_Center
gptkb:NASA
|
|
gptkbp:launch_price
|
$500 million
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
2
|
|
gptkbp:launch_window
|
gptkb:2021
|
|
gptkbp:manufacturer
|
gptkb:NASA
|
|
gptkbp:mission
|
gptkb:Artemis_I
gptkb:NASA_Mission_Control_Center
|
|
gptkbp:mission_type
|
Deep Space Exploration
|
|
gptkbp:number_of_engines
|
gptkb:4
|
|
gptkbp:number_of_stages
|
gptkb:Core_Stage
ICPS
|
|
gptkbp:objective
|
gptkb:Mars_missions
Lunar missions
|
|
gptkbp:operational_status
|
Active
|
|
gptkbp:orbital_altitude
|
7.8 km/s
|
|
gptkbp:payload_capacity
|
95 metric tons
|
|
gptkbp:propulsion
|
8.4 million pounds
|
|
gptkbp:safety_rating
|
gptkb:High
|
|
gptkbp:solid_rocket_booster_diameter
|
3.7 meters
|
|
gptkbp:solid_rocket_booster_length
|
45.2 meters
|
|
gptkbp:solid_rocket_booster_thrust
|
3.6 million pounds
|
|
gptkbp:sustainability_efforts
|
NASA Sustainability Program
|
|
gptkbp:upgrades
|
Block 1 B
|
|
gptkbp:bfsParent
|
gptkb:Artemis_II
|
|
gptkbp:bfsLayer
|
4
|