Statements (106)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Space_Shuttle
|
| gptkbp:academic_programs |
comprised of skilled engineers and scientists
|
| gptkbp:budget |
billions of dollars
|
| gptkbp:challenges |
radiation protection
faces engineering challenges |
| gptkbp:collaboration |
gptkb:European_Space_Agency
gptkb:ESA_(European_Space_Agency) |
| gptkbp:communication_system |
gptkb:NASA's_Space_Network
high-data-rate communication system |
| gptkbp:community_engagement |
educational outreach programs
engages public interest in space exploration |
| gptkbp:control_system |
fly-by-wire control system
|
| gptkbp:cooling_system |
gptkb:Avcoat
ablative heat shield |
| gptkbp:crew |
gptkb:Johnson_Space_Center
gptkb:Launch_Escape_System biometric sensors extensive training required prioritizes crew safety monitors crew health during missions |
| gptkbp:crew_capacity |
gptkb:4
4 astronauts |
| gptkbp:current_status |
in development
|
| gptkbp:design |
gptkb:multi-purpose_crew_vehicle
gptkb:Lockheed_Martin 21 days underwent multiple design iterations |
| gptkbp:developed_by |
gptkb:NASA
|
| gptkbp:development |
gptkb:2006
drives technology development |
| gptkbp:diameter |
approximately 15.2 feet
|
| gptkbp:durability |
limited reusability
|
| gptkbp:emergency_services |
abort scenarios
|
| gptkbp:environmental_impact |
thermal vacuum tests
|
| gptkbp:first_flight |
gptkb:2014
gptkb:Ascent_Abort-2 conducted test flights prior to crewed missions extensive spacecraft testing required |
| gptkbp:first_uncrewed_test_flight |
gptkb:Exploration_Flight_Test-1
|
| gptkbp:fuel_type |
liquid oxygen and liquid hydrogen
|
| gptkbp:funding |
federal budget allocations
funded by public taxpayer dollars |
| gptkbp:future_plans |
gptkb:Mars_missions
|
| gptkbp:has_documentation |
NASA Technical Reports Server
|
| gptkbp:historical_significance |
significant for future space exploration
first crewed spacecraft since Apollo |
| https://www.w3.org/2000/01/rdf-schema#label |
Orion spacecraft program
|
| gptkbp:is_integrated_with |
gptkb:Orion_Multi-Purpose_Crew_Vehicle
|
| gptkbp:is_tested_for |
ongoing
|
| gptkbp:launch_date |
once every 2-3 years
planned for multiple launches subject to launch schedule adjustments |
| gptkbp:launch_site |
gptkb:Kennedy_Space_Center
|
| gptkbp:launch_vehicle |
gptkb:Space_Launch_System
|
| gptkbp:launch_window |
specific launch windows required
every 18 months |
| gptkbp:length |
approximately 16.5 feet
|
| gptkbp:life_support_system |
closed-loop system
advanced life support system |
| gptkbp:mission |
gptkb:Artemis_I
gptkb:Houston,_Texas gptkb:NASA_Mission_Control_Center planned for Mars missions |
| gptkbp:mission_duration |
capable of long-duration missions
|
| gptkbp:mission_type |
crewed missions
|
| gptkbp:module |
crew module
|
| gptkbp:navigation_system |
gptkb:Inertial_Navigation_System
advanced avionics |
| gptkbp:objective |
gptkb:Mars_exploration
return humans to the Moon |
| gptkbp:orbital_altitude |
low Earth orbit
capable of orbital operations |
| gptkbp:partnerships |
various industry partners
commercial spaceflight companies |
| gptkbp:payload_capacity |
up to 10 tons
capable of carrying significant payloads |
| gptkbp:planned_missions |
gptkb:Artemis_program
|
| gptkbp:price |
$23 billion
|
| gptkbp:project |
2020s to 2030s
regular project updates provided long-term project timeline NASA Exploration Systems Development aims to expand human presence in space focus on developing future technologies managed by NASA's Exploration Systems Development |
| gptkbp:purpose |
deep space exploration
|
| gptkbp:research |
microgravity experiments
supports scientific research missions |
| gptkbp:return_capabilities |
capable of returning from deep space
|
| gptkbp:reviews |
Preliminary Design Review
subject to engineering reviews |
| gptkbp:safety_features |
gptkb:launch_escape_system
|
| gptkbp:safety_measures |
static fire tests
extensive safety testing conducted |
| gptkbp:simulator |
Orion crew training simulator
|
| gptkbp:spacecraft |
crew spacecraft
includes multiple advanced components includes recovery operations post-mission |
| gptkbp:speed |
25,000 mph
|
| gptkbp:sustainability |
reusable components
focus on sustainable exploration |
| gptkbp:sustainability_efforts |
reduce space debris
|
| gptkbp:training_programs |
virtual reality systems
|
| gptkbp:weight |
approximately 22,000 pounds
|
| gptkbp:year |
gptkb:2006
ongoing |