|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:budget
|
$20 billion
|
|
gptkbp:capacity
|
4 astronauts
|
|
gptkbp:cargo_capacity
|
up to 1,000 kg
|
|
gptkbp:collaboration
|
gptkb:ESA_(European_Space_Agency)
ESA, JAXA
|
|
gptkbp:communication_system
|
S-band and Ku-band
high-frequency radio
|
|
gptkbp:community_engagement
|
outreach programs for education
|
|
gptkbp:control_system
|
fly-by-wire system
|
|
gptkbp:cooling_system
|
gptkb:Avcoat
ablative heat shield
|
|
gptkbp:crew
|
gptkb:launch_escape_system
gptkb:NASA_Astronauts
high safety standards
launch abort system
supports crew health and safety
NASA astronaut training program
habitable crew module
|
|
gptkbp:crew_capacity
|
gptkb:4
4 to 6 astronauts
|
|
gptkbp:crew_training_facility
|
gptkb:Johnson_Space_Center
|
|
gptkbp:design
|
15 years
Lockheed Martin and NASA
|
|
gptkbp:design_features
|
modular design
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:designed_for
|
gptkb:human_spaceflight
crewed missions to the Moon and Mars
|
|
gptkbp:development
|
gptkb:2006
|
|
gptkbp:diameter
|
4.5 meters
|
|
gptkbp:emergency_services
|
regular safety drills for crew
NASA emergency protocols
|
|
gptkbp:environmental_concerns
|
temperature and humidity control system
|
|
gptkbp:environmental_impact
|
vacuum and thermal testing
|
|
gptkbp:first_flight
|
gptkb:Artemis_II
gptkb:2014
gptkb:Exploration_Flight_Test-1
2014-12-05
ongoing testing and evaluation
|
|
gptkbp:height
|
3 meters
|
|
gptkbp:historical_significance
|
part of Artemis lunar exploration program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Orion Multi-Purpose Crew Vehicle
|
|
gptkbp:integrates_with
|
gptkb:Space_Launch_System
|
|
gptkbp:is_explored_in
|
Mars and beyond
|
|
gptkbp:is_integrated_with
|
gptkb:NASA's_Kennedy_Space_Center
|
|
gptkbp:is_tested_for
|
development and testing
ground testing and simulations
|
|
gptkbp:landing_distance
|
splashdown
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Space_Launch_System
|
|
gptkbp:launch_window
|
flexible launch windows
depends on mission profile
|
|
gptkbp:launched
|
extensive pre-launch checks
|
|
gptkbp:length
|
5 meters
|
|
gptkbp:life_support_system
|
closed-loop system
environmental control and life support system
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
gptkb:NASA
|
|
gptkbp:mass
|
22,000 kg
|
|
gptkbp:mission
|
gptkb:Artemis_program
gptkb:NASA_Johnson_Space_Center
gptkb:NASA_Mission_Control_Center
detailed mission debriefs
|
|
gptkbp:mission_duration
|
up to 21 days
|
|
gptkbp:mission_type
|
deep space exploration
|
|
gptkbp:navigation_system
|
gptkb:navigation_system
gptkb:Inertial_Navigation_System
|
|
gptkbp:objective
|
support missions to the Moon and Mars
|
|
gptkbp:operational_since
|
gptkb:2014
gptkb:2020
|
|
gptkbp:operational_use
|
deep space missions
crewed missions to Moon and Mars
|
|
gptkbp:orbital_altitude
|
up to 1000 km
capable of orbital maneuvers
up to 5,000 km
|
|
gptkbp:payload_capacity
|
up to 10,000 kg
up to 1,000 kg to lunar orbit
|
|
gptkbp:power_source
|
solar panels
solar power
|
|
gptkbp:propulsion
|
gptkb:Orion_Service_Module
|
|
gptkbp:provides_information_on
|
high-data-rate communication system
|
|
gptkbp:purpose
|
crewed deep space exploration
|
|
gptkbp:recovery_method
|
ocean splashdown
|
|
gptkbp:safety_features
|
gptkb:launch_escape_system
|
|
gptkbp:safety_measures
|
extensive safety tests
|
|
gptkbp:safety_rating
|
NASA safety standards
|
|
gptkbp:spacecraft
|
multiple configurations available
crew spacecraft
|
|
gptkbp:speed
|
gptkb:shield
up to 40,000 km/h
|
|
gptkbp:sustainability
|
reusable components
two deployable solar arrays
|
|
gptkbp:sustainability_features
|
recyclable materials
|
|
gptkbp:upgrades
|
planned upgrades for Mars missions
|
|
gptkbp:width
|
4 meters
|
|
gptkbp:bfsParent
|
gptkb:Apollo_Lunar_Module
gptkb:Aerojet_Rocketdyne
gptkb:Artemis_I
gptkb:Kennedy_Space_Center
gptkb:Ames_Research_Center
gptkb:Glenn_Research_Center
|
|
gptkbp:bfsLayer
|
4
|