|
gptkbp:instance_of
|
gptkb:Space_Launch_System
|
|
gptkbp:academic_programs
|
multidisciplinary
NASA engineers and contractors
|
|
gptkbp:block
|
Block 1
|
|
gptkbp:built
|
gptkb:NASA
|
|
gptkbp:challenges
|
high complexity
weight and aerodynamics
|
|
gptkbp:collaborates_with
|
gptkb:European_Space_Agency
gptkb:Lockheed_Martin
gptkb:Northrop_Grumman
gptkb:Boeing
|
|
gptkbp:collaboration
|
gptkb:ESA
collaborations with other space agencies
|
|
gptkbp:community_engagement
|
outreach programs
STEM education initiatives
|
|
gptkbp:configuration
|
Block 1
Block 2
Block 1 B
|
|
gptkbp:crew
|
trained astronauts
|
|
gptkbp:crew_capacity
|
4 astronauts
up to 4 astronauts
|
|
gptkbp:critical_design_review
|
completed in 2016
|
|
gptkbp:design
|
gptkb:Northrop_Grumman
15 launches
|
|
gptkbp:design_purpose
|
send humans to Mars
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:designed_for
|
deep space exploration
|
|
gptkbp:developed_by
|
gptkb:NASA
|
|
gptkbp:development
|
gptkb:2011
gptkb:NASA
|
|
gptkbp:development_cost
|
$18 billion
|
|
gptkbp:diameter
|
8.4 meters
|
|
gptkbp:durability
|
partially reusable
|
|
gptkbp:engine
|
gptkb:NASA's_Marshall_Space_Flight_Center
|
|
gptkbp:engine_type
|
gptkb:RS-25
|
|
gptkbp:engineering_documentation
|
extensive records
|
|
gptkbp:environmental_impact
|
assessed
NASA's environmental assessments
|
|
gptkbp:facilities
|
gptkb:Stennis_Space_Center
gptkb:NASA's_Michoud_Assembly_Facility
|
|
gptkbp:features
|
advanced avionics
reusable components
|
|
gptkbp:first_flight
|
gptkb:Artemis_I
gptkb:2021
Green Run
|
|
gptkbp:fuel_type
|
liquid hydrogen and liquid oxygen
liquid oxygen
liquid hydrogen
|
|
gptkbp:funding
|
government budget allocations
U. S. government budget
|
|
gptkbp:future_block
|
Block 2
|
|
gptkbp:future_exploration_goals
|
return humans to the Moon
|
|
gptkbp:future_goals
|
sustainable lunar presence
|
|
gptkbp:has_component
|
gptkb:Orion_Spacecraft
gptkb:Core_Stage
gptkb:Solid_Rocket_Boosters
gptkb:Interim_Cryogenic_Propulsion_Stage
Launch Platform
|
|
gptkbp:has_mission
|
gptkb:Artemis_program
|
|
gptkbp:has_programs
|
active
|
|
gptkbp:has_test_facility
|
gptkb:NASA's_Kennedy_Space_Center
gptkb:NASA's_Stennis_Space_Center
gptkb:NASA's_Michoud_Assembly_Facility
|
|
gptkbp:height
|
98 meters
|
|
gptkbp:historical_achievement
|
critical design review, first flight
|
|
gptkbp:historical_significance
|
successor to Space Shuttle
first step to Mars missions
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
NASA's Space Launch System
|
|
gptkbp:infrastructure
|
Mobile Launcher
|
|
gptkbp:innovation
|
new materials and technologies
|
|
gptkbp:integration
|
gptkb:Vehicle_Assembly_Building
approximately 12 months
|
|
gptkbp:involved_technology
|
gptkb:Orion_spacecraft
|
|
gptkbp:is_a_supporter_of
|
planned
|
|
gptkbp:is_designed_for
|
gptkb:human_spaceflight
cargo missions
|
|
gptkbp:is_funded_by
|
gptkb:U._S._Government
|
|
gptkbp:is_part_of
|
gptkb:Artemis_program
|
|
gptkbp:is_supported_by
|
gptkb:NASA's_Artemis_program
gptkb:NASA's_Exploration_Systems_Development
gptkb:NASA's_Space_Technology_Mission_Directorate
|
|
gptkbp:is_tested_for
|
gptkb:NASA's_Kennedy_Space_Center
gptkb:2021
gptkb:NASA's_Stennis_Space_Center
gptkb:NASA's_Michoud_Assembly_Facility
|
|
gptkbp:is_used_for
|
gptkb:robotic_missions
scientific exploration
crew missions
interplanetary missions
lunar missions
|
|
gptkbp:launch_date
|
2024
1-2 per year
2024 for Artemis II
once every 2-3 years
|
|
gptkbp:launch_platform
|
gptkb:Launch_Complex_39_B
gptkb:NASA's_Launch_Services_Program
|
|
gptkbp:launch_price
|
$2 billion per launch
estimated $2 billion per launch
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
2
two
|
|
gptkbp:launch_window
|
2020s
varies by mission
specific mission timelines
|
|
gptkbp:launched
|
extensive testing
months of pre-launch activities
|
|
gptkbp:lifespan
|
20 years
|
|
gptkbp:manufacturer
|
gptkb:Boeing
|
|
gptkbp:mission
|
gptkb:Johnson_Space_Center
gptkb:Artemis_I
gptkb:Artemis_II
gptkb:Mars_missions
gptkb:NASA's_Johnson_Space_Center
high
Artemis II, Artemis III
validate design and performance
Moon missions
critical for NASA's goals
|
|
gptkbp:mission_type
|
crewed and uncrewed
|
|
gptkbp:notable_mission
|
gptkb:Artemis_program
|
|
gptkbp:number_of_stages
|
liquid hydrogen and liquid oxygen
4 engines
|
|
gptkbp:operational_since
|
gptkb:2021
|
|
gptkbp:orbital_altitude
|
up to 28,000 km/h
|
|
gptkbp:partnerships
|
gptkb:commercial_space_companies
|
|
gptkbp:payload_capacity
|
up to 130 metric tons
up to 130 tons
|
|
gptkbp:project
|
gptkb:John_Honeycutt
gptkb:NASA's_Artemis_program_office
over a decade
in-space propulsion
|
|
gptkbp:projected_operational_life
|
20 years
|
|
gptkbp:propulsion
|
8.4 million pounds
|
|
gptkbp:public_interest
|
high
high due to space exploration goals
|
|
gptkbp:purpose
|
deep space exploration
|
|
gptkbp:released_in
|
gptkb:2011
|
|
gptkbp:replaces
|
gptkb:Space_Shuttle
|
|
gptkbp:reusable_components
|
no
|
|
gptkbp:safety_features
|
multiple redundancy systems
multiple redundancy
|
|
gptkbp:safety_measures
|
static fire tests
NASA standards
|
|
gptkbp:scientific_goals
|
gptkb:Mars_exploration
|
|
gptkbp:specification
|
detailed engineering documents
|
|
gptkbp:successor
|
gptkb:Space_Shuttle
|
|
gptkbp:support
|
gptkb:Artemis_missions
|
|
gptkbp:supports
|
custom-built
|
|
gptkbp:sustainability_efforts
|
reduce carbon footprint
|
|
gptkbp:upgrades
|
gptkb:advanced_propulsion_systems
Block 1 B configuration
|
|
gptkbp:bfsParent
|
gptkb:Cape_Canaveral
gptkb:Commercial_Crew_Program
gptkb:Artemis_I
gptkb:NASA_Stennis_Space_Center
gptkb:Sierra_Nevada_Corporation
gptkb:NASA_Kennedy_Space_Center
gptkb:The_Kennedy_Space_Center
gptkb:Space_Launch_System_(SLS)
|
|
gptkbp:bfsLayer
|
4
|