|
gptkbp:instance_of
|
gptkb:planet
|
|
gptkbp:bfsLayer
|
3
|
|
gptkbp:bfsParent
|
gptkb:Space_X
gptkb:NASA
|
|
gptkbp:budget
|
several billion dollars
|
|
gptkbp:challenges
|
landing on the Moon
|
|
gptkbp:collaborations
|
private aerospace companies
various space agencies
international space community
|
|
gptkbp:communication
|
high-frequency radio
|
|
gptkbp:community_engagement
|
high
outreach programs
|
|
gptkbp:crew
|
gptkb:4
ongoing
|
|
gptkbp:design
|
currently in development
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:developed_by
|
gptkb:Human_Landing_System_program
|
|
gptkbp:developer
|
2020-2025
|
|
gptkbp:educational_programs
|
multidisciplinary team
|
|
gptkbp:elevation
|
gptkb:battle
|
|
gptkbp:environment
|
lunar environment
|
|
gptkbp:environmental_impact
|
minimized
|
|
gptkbp:exhibited_at
|
new lunar technologies
|
|
gptkbp:facilities
|
NASA centers
|
|
gptkbp:first_flight
|
2024
planned for 2023
|
|
gptkbp:fuel_type
|
liquid oxygen and hydrogen
|
|
gptkbp:game_world
|
gptkb:battle
|
|
gptkbp:height
|
approximately 7 meters
|
|
gptkbp:historical_significance
|
return to the Moon
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Artemis lunar lander
|
|
gptkbp:instrument
|
various payloads
|
|
gptkbp:key
|
modular design
|
|
gptkbp:landing_site
|
lunar surface
|
|
gptkbp:launch_date
|
every few years
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:software
|
|
gptkbp:launched
|
extensive
2024-2025
|
|
gptkbp:max_takeoff_weight
|
precision landing
|
|
gptkbp:mission
|
gptkb:Mars_exploration
gptkb:Artemis_program
gptkb:battle
sustained lunar presence
explore lunar south pole
|
|
gptkbp:mission_duration
|
up to 14 days
|
|
gptkbp:navigation_system
|
autonomous navigation
|
|
gptkbp:operational_status
|
in development
|
|
gptkbp:part_of
|
gptkb:Artemis_I_mission
|
|
gptkbp:power_output
|
solar panels
|
|
gptkbp:project
|
NASA leadership
|
|
gptkbp:provides_information_on
|
splashdown
|
|
gptkbp:purpose
|
gptkb:planet
|
|
gptkbp:released
|
2025
|
|
gptkbp:safety_features
|
conducted
redundant systems
stringent
NASA standards
|
|
gptkbp:scientific_goals
|
gptkb:software
|
|
gptkbp:seating_capacity
|
up to 1,000 kg
|
|
gptkbp:sustainability
|
designed for long-term missions
|
|
gptkbp:sustainability_initiatives
|
support human exploration
|
|
gptkbp:technology
|
gptkb:robot
advanced propulsion
|
|
gptkbp:weight
|
approximately 15,000 pounds
|
|
gptkbp:width
|
approximately 4 meters
|