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gptkbp:instance_of
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gptkb:spacecraft
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gptkbp:bfsLayer
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3
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gptkbp:bfsParent
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gptkb:Orion
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gptkbp:challenges
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overcoming technical hurdles
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gptkbp:collaborations
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ESA and JAXA
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gptkbp:communication
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advanced telemetry and tracking
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gptkbp:community_engagement
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educational outreach programs
|
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gptkbp:crew
|
biometric sensors
4 to 6 astronauts
NASA astronaut selection process
simulator training programs
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|
gptkbp:design
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completed in 2011
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gptkbp:developed_by
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gptkb:NASA
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gptkbp:diameter
|
approximately 5 meters
|
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gptkbp:durability
|
gptkb:theorem
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|
gptkbp:elevation
|
up to 1,000 km
|
|
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: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:is_designed_for
|
gptkb:spacecraft
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:software
|
|
gptkbp:launched
|
determined by mission objectives
|
|
gptkbp:length
|
approximately 4.5 meters
|
|
gptkbp:max_takeoff_weight
|
parachute and airbag system
|
|
gptkbp:mission
|
gptkb:Johnson_Space_Center
gptkb:Artemis_program
data collection and review
high success rate expected
exploration of the Moon and Mars
|
|
gptkbp:mission_duration
|
up to 21 days
|
|
gptkbp:navigation_system
|
gptkb:hospital
|
|
gptkbp:operating_system
|
custom flight software
|
|
gptkbp:operational_status
|
gptkb:2020
|
|
gptkbp:partnerships
|
commercial spaceflight companies
|
|
gptkbp:power_output
|
solar panels
|
|
gptkbp:project
|
incorporating new advancements
|
|
gptkbp:receives_funding_from
|
funded by U. S. government
|
|
gptkbp:research_interest
|
scientific experiments in microgravity
|
|
gptkbp:safety_features
|
gptkb:aircraft
NASA's safety standards
|
|
gptkbp:scholarships
|
closed-loop system
|
|
gptkbp:seating_capacity
|
modular design
up to 1,000 kg
|
|
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
|