|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:cargo_capacity
|
up to 1,000 kg
|
|
gptkbp:challenges
|
overcoming technical hurdles
|
|
gptkbp:collaboration
|
ESA and JAXA
|
|
gptkbp:communication_system
|
advanced telemetry and tracking
|
|
gptkbp:community_engagement
|
educational outreach programs
|
|
gptkbp:crew
|
biometric sensors
NASA astronaut selection process
simulator training programs
|
|
gptkbp:crew_capacity
|
4 to 6 astronauts
|
|
gptkbp:design
|
completed in 2011
|
|
gptkbp:designed_for
|
gptkb:human_spaceflight
|
|
gptkbp:developed_by
|
gptkb:NASA
|
|
gptkbp:diameter
|
approximately 5 meters
|
|
gptkbp:durability
|
gptkb:true
|
|
gptkbp:emergency_services
|
regularly conducted
comprehensive training
|
|
gptkbp:environmental_impact
|
thermal vacuum tests
|
|
gptkbp:facilities
|
gptkb:NASA_Langley_Research_Center
|
|
gptkbp:first_flight
|
gptkb:2014
|
|
gptkbp:funding
|
funded by U. S. government
|
|
gptkbp:historical_significance
|
part of U. S. space exploration history
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
multi-purpose crew vehicle
|
|
gptkbp:inspiration
|
inspiring future generations of explorers
|
|
gptkbp:invention
|
gptkb:Orion_Exploration_Flight_Test-1
|
|
gptkbp:is_capable_of
|
deep space missions
|
|
gptkbp:landing_distance
|
parachute and airbag system
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Space_Launch_System
|
|
gptkbp:launch_window
|
determined by mission objectives
|
|
gptkbp:length
|
approximately 4.5 meters
|
|
gptkbp:life_support_system
|
closed-loop system
|
|
gptkbp:mission
|
gptkb:Johnson_Space_Center
gptkb:Artemis_program
data collection and review
high success rate expected
|
|
gptkbp:mission_duration
|
up to 21 days
|
|
gptkbp:navigation_system
|
gptkb:navigation_system
|
|
gptkbp:operational_since
|
gptkb:2020
|
|
gptkbp:orbital_altitude
|
up to 1,000 km
|
|
gptkbp:partnerships
|
commercial spaceflight companies
|
|
gptkbp:payload_capacity
|
modular design
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:primary_mission
|
exploration of the Moon and Mars
|
|
gptkbp:project
|
incorporating new advancements
|
|
gptkbp:research_opportunities
|
scientific experiments in microgravity
|
|
gptkbp:safety_features
|
gptkb:launch_escape_system
|
|
gptkbp:safety_rating
|
NASA's safety standards
|
|
gptkbp:software_system
|
custom flight software
|
|
gptkbp:speed
|
up to 28,000 km/h
|
|
gptkbp:sustainability
|
focus on long-duration missions
|
|
gptkbp:used_in
|
gptkb:Orion_program
|
|
gptkbp:weight
|
approximately 22,000 kg
|
|
gptkbp:bfsParent
|
gptkb:Artemis_I
gptkb:Orion
|
|
gptkbp:bfsLayer
|
4
|