Statements (65)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:spacecraft
|
| gptkbp:capacity |
4 astronauts
|
| gptkbp:challenges |
overcame significant engineering challenges
|
| gptkbp:collaboration |
gptkb:ESA_(European_Space_Agency)
|
| gptkbp:communication_system |
high-data-rate communication
|
| gptkbp:community_engagement |
public outreach programs
|
| gptkbp:control_system |
fly-by-wire system
|
| gptkbp:cooling_system |
ablative heat shield
|
| gptkbp:crew |
integrated launch escape system
designed for crew comfort during missions extensive astronaut training required prioritizes crew safety in design |
| gptkbp:crew_capacity |
up to 6 astronauts
|
| gptkbp:design |
gptkb:multi-purpose_crew_vehicle
15 years modular components for upgrades |
| gptkbp:development |
gptkb:Orion_program
|
| gptkbp:development_cost |
approximately $20 billion
|
| gptkbp:diameter |
15.2 feet
|
| gptkbp:durability |
limited reusability
|
| gptkbp:emergency_services |
regular safety drills conducted
|
| gptkbp:environmental_impact |
extensive environmental testing conducted
|
| gptkbp:first_flight |
gptkb:2014
multiple test flights planned |
| gptkbp:funding |
funded by U. S. government
|
| gptkbp:future_plans |
future missions to Mars planned
|
| gptkbp:historical_significance |
part of NASA's Artemis program
|
| https://www.w3.org/2000/01/rdf-schema#label |
Orion crew vehicle
|
| gptkbp:improves |
ongoing design improvements based on testing
|
| gptkbp:is_explored_in |
key to future exploration of the Moon and Mars
|
| gptkbp:is_tested_for |
ongoing
|
| gptkbp:landing_distance |
parachute-assisted landing
|
| gptkbp:launch_date |
planned for regular launches
|
| gptkbp:launch_site |
gptkb:Kennedy_Space_Center
|
| gptkbp:launch_vehicle |
gptkb:Space_Launch_System
|
| gptkbp:length |
16.5 feet
|
| gptkbp:life_support_system |
closed-loop life support
|
| gptkbp:manufacturer |
gptkb:NASA
|
| gptkbp:mission |
gptkb:Artemis_I
gptkb:Exploration_Flight_Test-1 gptkb:Artemis_program gptkb:NASA_Mission_Control_Center |
| gptkbp:mission_duration |
up to 21 days in space
|
| gptkbp:navigation_system |
advanced avionics
|
| gptkbp:operational_since |
gptkb:2020
|
| gptkbp:orbital_altitude |
capable of orbital maneuvers
up to 22,000 miles |
| gptkbp:partnerships |
collaborations with private aerospace companies
|
| gptkbp:payload_capacity |
up to 1,000 kg
|
| gptkbp:power_source |
solar panels
|
| gptkbp:project |
projected timeline for future missions
|
| gptkbp:projected_missions |
multiple missions to Moon and Mars
|
| gptkbp:purpose |
crewed deep space exploration
|
| gptkbp:research_opportunities |
scientific research opportunities during missions
|
| gptkbp:safety_features |
gptkb:launch_escape_system
|
| gptkbp:safety_rating |
high safety standards
|
| gptkbp:scientific_instruments |
equipped with scientific instruments for research
|
| gptkbp:spacecraft |
deep space crew vehicle
redundant spacecraft systems for reliability |
| gptkbp:spacecraft_integration |
integrated with other spacecraft systems
|
| gptkbp:speed |
25,000 mph
|
| gptkbp:sustainability |
designed for long-duration missions
|
| gptkbp:weight |
approximately 22,000 pounds
|
| gptkbp:bfsParent |
gptkb:Boeing
|
| gptkbp:bfsLayer |
4
|