gptkbp:instance_of
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gptkb:spacecraft
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gptkbp:budget
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$20 billion
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gptkbp:collaboration
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gptkb:NASA_and_ESA
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gptkbp:communication_system
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S-band and Ku-band
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gptkbp:community_engagement
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educational outreach programs
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gptkbp:control_system
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fly-by-wire
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gptkbp:cooling_system
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gptkb:Avcoat
ablative heat shield
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gptkbp:crew
|
ongoing
active during launch
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gptkbp:crew_capacity
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gptkb:4
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gptkbp:design
|
15 years
NASA engineers
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gptkbp:development
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gptkb:2006
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gptkbp:diameter
|
4.5 meters
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gptkbp:durability
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partially reusable
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gptkbp:entry_speed
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up to 25,000 km/h
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gptkbp:facilities
|
NASA facilities
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gptkbp:first_flight
|
gptkb:Exploration_Flight_Test-1
2014-12-05
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gptkbp:first_manned_mission
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2024
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gptkbp:fuel_type
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liquid oxygen and liquid hydrogen
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gptkbp:historical_significance
|
next step in human space exploration
|
https://www.w3.org/2000/01/rdf-schema#label
|
SV Orion
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gptkbp:is_a_destination_for
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gptkb:Moon
gptkb:Mars
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gptkbp:landing_distance
|
parachute and airbag system
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gptkbp:launch_date
|
every 2 years
2023-11-16
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gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
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gptkbp:launch_vehicle
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gptkb:Space_Launch_System
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gptkbp:launch_window
|
every 2 years
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gptkbp:length
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3.3 meters
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gptkbp:life_support_system
|
closed-loop system
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gptkbp:manufacturer
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gptkb:Lockheed_Martin
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gptkbp:mass
|
22,000 kg
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gptkbp:mission
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gptkb:Johnson_Space_Center
gptkb:Artemis_program
multi-phase missions
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gptkbp:mission_duration
|
up to 21 days
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gptkbp:navigation_system
|
gptkb:GPS
|
gptkbp:orbital_altitude
|
yes
up to 1000 km
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gptkbp:partnerships
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gptkb:commercial_space_companies
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gptkbp:payload_capacity
|
up to 10,000 kg
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gptkbp:power_source
|
solar panels
|
gptkbp:purpose
|
crewed deep space exploration
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gptkbp:safety_features
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gptkb:launch_escape_system
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gptkbp:safety_rating
|
high
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gptkbp:scientific_instruments
|
various payloads
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gptkbp:specification
|
available on NASA website
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gptkbp:speed
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up to 7 degrees
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gptkbp:status
|
in development
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gptkbp:sustainability
|
designed for long missions
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gptkbp:bfsParent
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gptkb:De_Treffers
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gptkbp:bfsLayer
|
8
|