|
instanceOf
|
NASA spacecraft
→
crewed spacecraft
→
space capsule
→
|
|
abortSystemType
|
launch escape system
→
|
|
ArtemisILaunchDate
|
2022-11-16
→
|
|
ArtemisIMissionType
|
uncrewed lunar test flight
→
|
|
ArtemisISplashdownDate
|
2022-12-11
→
|
|
communications
|
deep space communication systems
→
|
|
component
|
crew module
→
launch abort system
→
service module
→
|
|
countryOfOrigin
|
United States
→
|
|
crewCapacity
|
4 astronauts
→
|
|
crewCapacityMaximum
|
6 astronauts (short duration)
→
|
|
designedFor
|
crewed missions beyond low Earth orbit
→
future Mars missions
→
lunar missions
→
|
|
designedMissionDuration
|
up to 21 days with crew
→
|
|
dockingCapability
|
NASA Docking System compatible
→
|
|
firstCrewedFlight
|
Artemis II
→
|
|
firstFlight
|
2014-12-05
→
|
|
firstFlightMission
|
Exploration Flight Test 1
→
|
|
firstFlightType
|
uncrewed test flight
→
|
|
guidanceNavigationControl
|
advanced avionics and autonomous navigation
→
|
|
heatShieldType
|
ablative heat shield
→
|
|
intendedDestination
|
Mars (long-term goal)
→
Moon
→
cislunar space
→
|
|
launchVehicle
|
Delta IV Heavy (for EFT-1)
→
Space Launch System
→
|
|
lifeSupport
|
environmental control and life support system
→
|
|
manufacturer
|
Lockheed Martin Space
→
|
|
notableMission
|
Artemis I
→
|
|
operator
|
NASA
→
|
|
powerSource
|
solar arrays
→
|
|
previousProgramAssociation
|
Constellation program
→
|
|
primaryMission
|
deep space exploration
→
|
|
program
|
Artemis program
→
|
|
programGoal
|
enable sustained human presence beyond low Earth orbit
→
|
|
propulsionType
|
service module main engine and auxiliary thrusters
→
|
|
reentryCapability
|
high-speed reentry from lunar and deep-space trajectories
→
|
|
reentrySpeedCapability
|
approximately 11 km/s
→
|
|
serviceModuleManufacturer
|
Airbus Defence and Space
→
|
|
serviceModuleProvider
|
European Space Agency
→
|
|
spaceAgency
|
NASA
→
|
|
status
|
operational
→
|
|
successorTo
|
Apollo command and service module (role-wise)
→
|