|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:budget
|
$20 billion
|
|
gptkbp:challenges
|
thermal protection, avionics
|
|
gptkbp:collaboration
|
ESA, JAXA
|
|
gptkbp:communication_system
|
S-band and Ku-band
|
|
gptkbp:community_engagement
|
educational outreach programs
|
|
gptkbp:cooling_system
|
gptkb:Avcoat
|
|
gptkbp:crew
|
gptkb:NASA_Astronaut_Corps
yes
simulator-based training
real-time monitoring system
|
|
gptkbp:crew_capacity
|
gptkb:4
|
|
gptkbp:design
|
10 missions
Lockheed Martin, NASA engineers
|
|
gptkbp:development
|
gptkb:2006
|
|
gptkbp:diameter
|
4.5 meters
|
|
gptkbp:durability
|
partially reusable
|
|
gptkbp:emergency_services
|
regularly conducted
detailed protocols
|
|
gptkbp:environmental_impact
|
extensive testing phases
|
|
gptkbp:first_flight
|
gptkb:2023
gptkb:Exploration_Flight_Test-1
2014-12-05
|
|
gptkbp:fuel_type
|
liquid oxygen and hydrogen
|
|
gptkbp:funding
|
funded by U. S. government
|
|
gptkbp:historical_significance
|
first spacecraft designed for deep space missions since Apollo.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
NASA's Orion spacecraft
|
|
gptkbp:involved_technology
|
gptkb:advanced_propulsion_systems
|
|
gptkbp:landing_distance
|
splashdown
|
|
gptkbp:launch_date
|
2021-11-16
every few years
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Space_Launch_System
|
|
gptkbp:length
|
5 meters
|
|
gptkbp:life_support_system
|
closed-loop system
|
|
gptkbp:manufacturer
|
gptkb:NASA
|
|
gptkbp:mass
|
22,000 kg
|
|
gptkbp:mission
|
gptkb:Johnson_Space_Center
gptkb:Artemis_I
gptkb:Artemis_program
|
|
gptkbp:mission_duration
|
up to 21 days
|
|
gptkbp:mission_type
|
gptkb:exploration
|
|
gptkbp:navigation_system
|
gptkb:Inertial_Navigation_System
|
|
gptkbp:objective
|
Moon and Mars missions
|
|
gptkbp:operational_status
|
in development
|
|
gptkbp:orbital_altitude
|
autonomous and manual
100 km to 400,000 km
|
|
gptkbp:partnerships
|
gptkb:commercial_space_companies
|
|
gptkbp:payload_capacity
|
up to 10,000 kg
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:purpose
|
crewed deep space exploration
|
|
gptkbp:return_velocity
|
25,000 mph
|
|
gptkbp:safety_features
|
gptkb:launch_escape_system
|
|
gptkbp:safety_rating
|
high
|
|
gptkbp:scientific_instruments
|
various payloads
|
|
gptkbp:sensor
|
various scientific sensors
|
|
gptkbp:sustainability
|
designed for long-duration missions
|
|
gptkbp:bfsParent
|
gptkb:Cape_Canaveral
gptkb:Artemis_I
gptkb:Robert_J._Collier_Trophy
gptkb:Sierra_Nevada_Corporation
gptkb:Delta_IV_Heavy
|
|
gptkbp:bfsLayer
|
4
|