|
gptkbp:instance_of
|
gptkb:Space_Shuttle
|
|
gptkbp:budget
|
$30 billion through 2025
|
|
gptkbp:challenges
|
overcoming engineering challenges
|
|
gptkbp:collaboration
|
with ESA and other partners
|
|
gptkbp:communication_system
|
high-data-rate communication
|
|
gptkbp:community_engagement
|
engaging the public in space exploration.
|
|
gptkbp:crew
|
integrated launch escape system
monitoring crew health during missions
extensive crew training programs
|
|
gptkbp:crew_capacity
|
gptkb:4
|
|
gptkbp:design
|
gptkb:Lockheed_Martin
|
|
gptkbp:design_features
|
modular design
|
|
gptkbp:design_started
|
gptkb:2006
|
|
gptkbp:developed_by
|
gptkb:NASA
|
|
gptkbp:development_cost
|
approximately $18 billion
|
|
gptkbp:facilities
|
gptkb:NASA's_Johnson_Space_Center
|
|
gptkbp:first_flight
|
gptkb:Artemis_II
gptkb:2014
Exploration Mission-1
|
|
gptkbp:first_uncrewed_test_flight
|
gptkb:Exploration_Flight_Test-1
|
|
gptkbp:has_ability
|
support missions to Mars
|
|
gptkbp:historical_significance
|
continuation of human space exploration
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Orion program
|
|
gptkbp:inspiration
|
inspire future generations of explorers
|
|
gptkbp:launch_date
|
2022 for Artemis I
planned for every 1-2 years
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Space_Launch_System
|
|
gptkbp:launch_window
|
specific launch windows for missions
|
|
gptkbp:life_support_system
|
advanced life support
|
|
gptkbp:mission
|
gptkb:Artemis_I
Mars and beyond
|
|
gptkbp:mission_duration
|
up to 21 days
|
|
gptkbp:mission_type
|
deep space exploration
|
|
gptkbp:module
|
crew module
|
|
gptkbp:navigation_system
|
gptkb:NASA's_Space_Network
|
|
gptkbp:orbital_altitude
|
approximately 3,600 miles
capable of orbital maneuvers
|
|
gptkbp:part_of
|
gptkb:Artemis_program
|
|
gptkbp:partnerships
|
with commercial space companies
|
|
gptkbp:payload_capacity
|
up to 10 tons
|
|
gptkbp:project
|
testing future technologies for space travel
|
|
gptkbp:public_interest
|
high public interest
|
|
gptkbp:purpose
|
gptkb:human_spaceflight
|
|
gptkbp:recovery_method
|
parachute recovery system
|
|
gptkbp:return_capabilities
|
capable of returning to Earth safely
|
|
gptkbp:safety_features
|
gptkb:launch_escape_system
|
|
gptkbp:safety_measures
|
extensive safety testing
|
|
gptkbp:safety_record
|
focus on safety and reliability
|
|
gptkbp:scientific_goals
|
study asteroids and lunar surface
|
|
gptkbp:service
|
gptkb:European_Space_Agency
|
|
gptkbp:speed
|
25,000 mph
|
|
gptkbp:successor
|
gptkb:Apollo_program
|
|
gptkbp:sustainability
|
designed for multiple missions
|
|
gptkbp:weight
|
approximately 22,000 pounds
|
|
gptkbp:bfsParent
|
gptkb:Orion_spacecraft
gptkb:human_spaceflight_programs
|
|
gptkbp:bfsLayer
|
4
|