Properties (56)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:spacecraft
|
| gptkbp:collaboratedWith |
gptkb:European_Space_Agency
|
| gptkbp:communicationEquipment |
high-data-rate communication
|
| gptkbp:crew |
NASA_astronaut_training_program
|
| gptkbp:crewCapacity |
4
|
| gptkbp:design |
15 years
|
| gptkbp:designedFor |
gptkb:NASA's_Artemis_program
|
| gptkbp:developedBy |
gptkb:Lockheed_Martin
|
| gptkbp:dimensions |
4.5 meters in height
|
| gptkbp:electronicSystems |
radiation protection
|
| gptkbp:emissionsStandard |
NASA's_safety_and_performance_standards
|
| gptkbp:environmentalImpact |
ablative heat shield
temperature and humidity control |
| gptkbp:firstFlight |
gptkb:Exploration_Flight_Test-1
2014 |
| gptkbp:fuelType |
hypergolic propellants
|
| gptkbp:hasFunding |
funded_by_U.S._taxpayers
|
| gptkbp:hasPartnershipsWith |
collaborations with multiple countries
|
| gptkbp:historicalSignificance |
part of human space exploration history
|
| https://www.w3.org/2000/01/rdf-schema#label |
Orion Service Module
|
| gptkbp:includes |
propulsion system
|
| gptkbp:integration |
Orion Crew Module
full-scale system tests |
| gptkbp:launchDate |
scheduled for 2024
|
| gptkbp:launched |
every few years
|
| gptkbp:launchSite |
gptkb:Kennedy_Space_Center
|
| gptkbp:launchVehicle |
gptkb:Space_Launch_System_(SLS)
|
| gptkbp:missions |
gptkb:Johnson_Space_Center
up to 21 days |
| gptkbp:navigationEquipment |
inertial navigation system
|
| gptkbp:operationalRole |
supporting lunar missions
|
| gptkbp:orbitalInclination |
low_Earth_orbit_and_beyond
|
| gptkbp:payloadCapacity |
up to 1,000 kg
|
| gptkbp:powers |
solar arrays
|
| gptkbp:project |
return humans to the Moon
successful mission completions key development phases comprehensive technical reports identified and mitigated risks ongoing development since 2006 NASA_budget_allocations |
| gptkbp:provides |
life support systems
|
| gptkbp:publicAccess |
educational outreach programs
|
| gptkbp:safetyFeatures |
launch escape system
extensive ground testing |
| gptkbp:scientificName |
various payloads
|
| gptkbp:secondaryMission |
Artemis I, Artemis II
|
| gptkbp:speed |
approximately 40,000 km/h
|
| gptkbp:supplyChain |
global supply network
|
| gptkbp:supports |
deep space missions
|
| gptkbp:sustainability |
reusable components
|
| gptkbp:systemRequirements |
multiple backup systems
|
| gptkbp:team |
multidisciplinary engineering team
|
| gptkbp:technology |
advanced propulsion systems
detailed engineering documents |
| gptkbp:weight |
approximately 13,000 kg
|