|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:budget
|
$20 billion
|
|
gptkbp:collaboration
|
gptkb:ESA
|
|
gptkbp:communication_system
|
high-frequency radio
|
|
gptkbp:community_engagement
|
educational outreach programs
|
|
gptkbp:control_system
|
fly-by-wire system
|
|
gptkbp:cooling_system
|
gptkb:Avcoat
|
|
gptkbp:crew
|
gptkb:launch_escape_system
high safety standards maintained.
biomedical monitoring systems
NASA astronaut training program
|
|
gptkbp:crew_capacity
|
gptkb:4
|
|
gptkbp:debut
|
multiple test flights planned
|
|
gptkbp:design
|
15 years
Lockheed Martin and NASA engineers
|
|
gptkbp:design_purpose
|
gptkb:Mars_missions
|
|
gptkbp:development
|
gptkb:2006
|
|
gptkbp:emergency_services
|
detailed emergency protocols
|
|
gptkbp:environmental_impact
|
extensive testing phases
|
|
gptkbp:facilities
|
NASA facilities in Florida
|
|
gptkbp:first_flight
|
gptkb:2023
gptkb:Exploration_Flight_Test-1
2014-12-05
|
|
gptkbp:funding
|
funded by U. S. government
|
|
gptkbp:height
|
3.3 meters
|
|
gptkbp:historical_significance
|
successor to Apollo program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Orion Spacecraft
|
|
gptkbp:is_tested_for
|
full system integration tests
|
|
gptkbp:landing_distance
|
gptkb:parachute
|
|
gptkbp:launch_date
|
every few years
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Space_Launch_System
|
|
gptkbp:launch_window
|
specific launch windows based on mission
|
|
gptkbp:length
|
5 meters
|
|
gptkbp:life_support_system
|
advanced life support system
|
|
gptkbp:manufacturer
|
gptkb:NASA
|
|
gptkbp:mass
|
22,000 kg
|
|
gptkbp:mission
|
gptkb:Artemis_program
gptkb:NASA_Mission_Control_Center
|
|
gptkbp:mission_duration
|
up to 21 days
|
|
gptkbp:mission_type
|
gptkb:exploration
|
|
gptkbp:navigation_system
|
gptkb:navigation_system
|
|
gptkbp:objective
|
return humans to the Moon
explore Mars
|
|
gptkbp:operational_status
|
in development
|
|
gptkbp:orbital_altitude
|
Low Earth Orbit
|
|
gptkbp:partnerships
|
collaborations with private sector
|
|
gptkbp:payload_capacity
|
up to 10 tons
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:project
|
gptkb:advanced_propulsion_systems
|
|
gptkbp:purpose
|
crewed deep space exploration
|
|
gptkbp:recovery_method
|
ship recovery
|
|
gptkbp:safety_features
|
gptkb:launch_escape_system
|
|
gptkbp:safety_rating
|
NASA safety standards
|
|
gptkbp:sensor
|
various scientific instruments
|
|
gptkbp:software_system
|
custom flight software
|
|
gptkbp:spacecraft
|
gptkb:multi-purpose_crew_vehicle
|
|
gptkbp:speed
|
32,000 km/h
|
|
gptkbp:supports
|
specialized ground systems
|
|
gptkbp:sustainability_features
|
recyclable materials used
|
|
gptkbp:width
|
4 meters
|
|
gptkbp:bfsParent
|
gptkb:Ferengi
gptkb:NASA's_Space_Launch_System
|
|
gptkbp:bfsLayer
|
5
|