Properties (64)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:spacecraft
|
| gptkbp:aftermath |
performed by recovery teams
|
| gptkbp:communicationEquipment |
high-frequency radio
|
| gptkbp:communitySupport |
allows for upgrades
|
| gptkbp:coolingSystem |
Avcoat
|
| gptkbp:crew |
simulator training
secure communication channels biometric sensors |
| gptkbp:crewCapacity |
4
designed for astronaut comfort active during launch |
| gptkbp:crewSize |
NASA_astronaut_selection_process
|
| gptkbp:dataTransmission |
high-speed data links
|
| gptkbp:design |
15 years
|
| gptkbp:designedBy |
NASA
|
| gptkbp:diameter |
4.5 meters
|
| gptkbp:diedIn |
closed-loop system
|
| gptkbp:electronicSystems |
overcoming technical hurdles
|
| gptkbp:emergencyServices |
detailed protocols
|
| gptkbp:environmentalImpact |
ablative heat shield
|
| gptkbp:firstFlight |
gptkb:Exploration_Flight_Test-1
2014 |
| gptkbp:firstPublished |
Artemis II
|
| gptkbp:fuelType |
liquid oxygen and liquid hydrogen
|
| gptkbp:futurePlans |
Mars_missions_planned
|
| gptkbp:hasFunding |
funded_by_U.S._government
|
| gptkbp:historicalSignificance |
part_of_Artemis_program
|
| https://www.w3.org/2000/01/rdf-schema#label |
The Orion Spacecraft
|
| gptkbp:integration |
full system integration tests
|
| gptkbp:internationalCooperation |
gptkb:ESA
|
| gptkbp:landingGear |
parachute system
|
| gptkbp:launched |
every 2 years
planned every few years |
| gptkbp:launchSite |
gptkb:Kennedy_Space_Center
|
| gptkbp:launchVehicle |
gptkb:Space_Launch_System
|
| gptkbp:length |
5 meters
|
| gptkbp:manufacturer |
gptkb:Lockheed_Martin
|
| gptkbp:mission |
crewed missions
|
| gptkbp:missions |
gptkb:Johnson_Space_Center
up to 21 days explore_lunar_and_Martian_environments |
| gptkbp:missionsConducted |
aims for successful lunar missions
|
| gptkbp:navigationEquipment |
inertial navigation system
|
| gptkbp:operationalStatus |
2020
|
| gptkbp:orbitalInclination |
100 km
performed by onboard computers |
| gptkbp:partnerships |
collaborations with universities
|
| gptkbp:payloadCapacity |
up to 10 tons
|
| gptkbp:powers |
solar panels
|
| gptkbp:project |
ongoing development
|
| gptkbp:publicAccess |
educational outreach programs
|
| gptkbp:purpose |
deep space exploration
|
| gptkbp:safety |
NASA_safety_protocols
|
| gptkbp:safetyFeatures |
launch escape system
extensive testing high safety standards maintained |
| gptkbp:scientificName |
various payloads
|
| gptkbp:secondaryMission |
gptkb:Artemis_program
detailed mission reports |
| gptkbp:speed |
25,000 km/h
|
| gptkbp:sustainability |
reusable components
|
| gptkbp:technology |
development of new systems
|
| gptkbp:waterQuality |
vacuum and thermal tests
|
| gptkbp:weight |
22,000 kg
|