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gptkbp:instance_of
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gptkb:spacecraft
|
|
gptkbp:budget
|
billions of dollars for development and missions
|
|
gptkbp:capacity
|
4 astronauts
up to 4 astronauts
|
|
gptkbp:challenges
|
faced various engineering challenges during development
|
|
gptkbp:collaboration
|
gptkb:ESA_(European_Space_Agency)
|
|
gptkbp:communication_system
|
solar panels
high-data-rate communication
|
|
gptkbp:compatibility
|
life support systems
|
|
gptkbp:control_system
|
fly-by-wire control system
|
|
gptkbp:cooling_system
|
ablative heat shield
|
|
gptkbp:crew
|
extensive training required
|
|
gptkbp:crew_capacity
|
4 to 6 astronauts
|
|
gptkbp:crew_escape
|
crew escape capability during launch
|
|
gptkbp:design
|
15 years
modular design for upgrades
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:development
|
gptkb:2006
|
|
gptkbp:diameter
|
4.5 meters
|
|
gptkbp:durability
|
gptkb:true
|
|
gptkbp:environmental_concerns
|
environmental control and life support system
|
|
gptkbp:facilities
|
utilizes advanced testing facilities
|
|
gptkbp:first_flight
|
gptkb:2014
gptkb:Exploration_Flight_Test-1
|
|
gptkbp:has_research_areas
|
capable of conducting scientific research
|
|
gptkbp:historical_significance
|
part of NASA's Artemis program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Orion crew module
|
|
gptkbp:inspiration
|
inspired future generations of engineers and scientists
|
|
gptkbp:integration
|
integrated with the Space Launch System
|
|
gptkbp:is_explored_in
|
Mars and beyond
|
|
gptkbp:landing_distance
|
gptkb:parachute
|
|
gptkbp:landing_site
|
ocean or land
|
|
gptkbp:launch_date
|
every few years
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Space_Launch_System
|
|
gptkbp:length
|
5 meters
|
|
gptkbp:mass
|
around 22,000 kg
|
|
gptkbp:mission
|
gptkb:Artemis_program
|
|
gptkbp:mission_duration
|
up to 21 days
|
|
gptkbp:mission_type
|
crewed missions
|
|
gptkbp:navigation_system
|
advanced avionics
|
|
gptkbp:operational_since
|
gptkb:2020
|
|
gptkbp:partnerships
|
collaborations with private companies
|
|
gptkbp:propulsion
|
orbital maneuvering system
|
|
gptkbp:public_interest
|
high public interest in missions
|
|
gptkbp:purpose
|
deep space exploration
|
|
gptkbp:safety_features
|
gptkb:launch_escape_system
|
|
gptkbp:safety_measures
|
rigorous safety testing conducted
|
|
gptkbp:sensor
|
various scientific instruments
|
|
gptkbp:speed
|
up to 25,000 km/h
|
|
gptkbp:sustainability
|
designed for long-duration missions
|
|
gptkbp:bfsParent
|
gptkb:Artemis_I
|
|
gptkbp:bfsLayer
|
4
|