|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:capacity
|
4 astronauts
|
|
gptkbp:communicationEquipment
|
high-frequency radio
|
|
gptkbp:controls
|
fly-by-wire system
|
|
gptkbp:crew
|
NASA Astronaut Corps
|
|
gptkbp:crewCapacity
|
yes
4 to 6 astronauts
|
|
gptkbp:design
|
15 days in space
|
|
gptkbp:designedFor
|
human spaceflight
|
|
gptkbp:developedBy
|
NASA
|
|
gptkbp:diameter
|
4.5 meters
|
|
gptkbp:diedIn
|
advanced life support
|
|
gptkbp:emergencyServices
|
ocean or land
|
|
gptkbp:environmentalImpact
|
ablative heat shield
|
|
gptkbp:firstFlight
|
gptkb:Exploration_Flight_Test-1
2014
planned for 2024
|
|
gptkbp:future_plans
|
upgrades planned for next missions
|
|
gptkbp:futurePlans
|
Lunar_Gateway_missions
|
|
gptkbp:historicalSignificance
|
next step in human space exploration.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Orion crew vehicle
|
|
gptkbp:inspiration
|
gptkb:Apollo_program
|
|
gptkbp:internationalCooperation
|
with_ESA_and_other_agencies
|
|
gptkbp:landingGear
|
parachute system
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launchVehicle
|
gptkb:Space_Launch_System
|
|
gptkbp:length
|
5 meters
|
|
gptkbp:mission
|
deep space exploration
|
|
gptkbp:navigationEquipment
|
inertial navigation system
|
|
gptkbp:operationalStatus
|
2020
|
|
gptkbp:orbitalInclination
|
up to 1000 km
|
|
gptkbp:payloadCapacity
|
up to 1,000 kg
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:primaryMission
|
gptkb:Artemis_program
|
|
gptkbp:producedBy
|
gptkb:Lockheed_Martin
|
|
gptkbp:publicAccess
|
high due to Artemis program
|
|
gptkbp:reliability
|
partially
|
|
gptkbp:returnPolicy
|
up to 25,000 km/h
|
|
gptkbp:safetyFeatures
|
ongoing
launch escape system
|
|
gptkbp:sensors
|
various scientific instruments
|
|
gptkbp:services
|
gptkb:European_Space_Agency
|
|
gptkbp:supports
|
Mars_exploration
|
|
gptkbp:sustainability
|
designed for long-duration missions
|
|
gptkbp:team
|
NASA_engineers_and_contractors
|
|
gptkbp:weight
|
22,000 kg
|