Statements (248)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:spacecraft
|
| gptkbp:artwork |
gptkb:Pacific_Ocean
gptkb:ocean |
| gptkbp:autonomous_operations |
yes
|
| gptkbp:budget |
$20 billion
|
| gptkbp:capacity |
4 astronauts
approximately 330 cubic feet |
| gptkbp:cargo_capacity |
up to 1,000 kg
|
| gptkbp:challenges |
overcoming technical hurdles
faced engineering challenges during development overcome through testing |
| gptkbp:client |
Boeing, Northrop Grumman
|
| gptkbp:collaboration |
gptkb:ESA
gptkb:ESA_(European_Space_Agency) ESA, JAXA ESA and NASA collaboration with ESA |
| gptkbp:communication_system |
gptkb:NASA's_Space_Network
S-band and Ku-band S-band and UHF high-frequency radio advanced communication system nuclear power system |
| gptkbp:community_engagement |
gptkb:public_engagement_initiatives
outreach programs educational outreach programs NASA's outreach programs NASA outreach programs |
| gptkbp:community_outreach |
educational outreach programs
|
| gptkbp:control_system |
Fly-by-wire system
fly-by-wire system |
| gptkbp:cooling_system |
gptkb:Avcoat
yes ablative heat shield |
| gptkbp:crew |
gptkb:NASA_Astronaut_Training_Program
gptkb:NASA_Astronaut_Corps gptkb:launch_escape_system yes simulator training extensive life support systems secure channels high priority launch abort system integrated crew escape system extensive crew training programs sleeping quarters and galley life support for astronauts |
| gptkbp:crew_capacity |
gptkb:4
4 astronauts 4 to 6 astronauts |
| gptkbp:current_status |
in development
|
| gptkbp:data_return |
capable of returning from deep space
|
| gptkbp:debut |
gptkb:2014
|
| gptkbp:deployment |
gptkb:NASA
|
| gptkbp:design |
gptkb:Lockheed_Martin
10 years 15 years ongoing completed in 2011 comprised of engineers and scientists 15 days in space Lockheed Martin and NASA |
| gptkbp:design_features |
modular design
|
| gptkbp:design_purpose |
exploration beyond low Earth orbit
|
| gptkbp:designed_by |
gptkb:NASA
|
| gptkbp:designed_for |
deep space exploration
deep space missions |
| gptkbp:developed_by |
gptkb:NASA
|
| gptkbp:development |
gptkb:2006
|
| gptkbp:development_cost |
$18 billion
estimated at $20 billion |
| gptkbp:diameter |
5 meters
4.5 meters 15.2 feet |
| gptkbp:emergency_services |
detailed emergency procedures
|
| gptkbp:facilities |
gptkb:NASA's_Johnson_Space_Center
NASA facilities |
| gptkbp:features |
launch abort system
|
| gptkbp:first_flight |
gptkb:Artemis_I
gptkb:Artemis_II gptkb:2014 gptkb:2023 gptkb:Exploration_Flight_Test-1 2024 2014-12-05 December 5, 2014 multiple test flights planned |
| gptkbp:fuel_type |
liquid oxygen and hydrogen
hypergolic propellant |
| gptkbp:has_programs |
gptkb:Constellation_program
gptkb:Orion_program gptkb:Artemis_program |
| gptkbp:height |
4.5 meters
|
| gptkbp:historical_significance |
historical significance in space exploration
first spacecraft designed for deep space missions since Apollo. part of Artemis program successor to Apollo spacecraft. |
| https://www.w3.org/2000/01/rdf-schema#label |
Orion spacecraft
|
| gptkbp:inspiration |
gptkb:Apollo_program
|
| gptkbp:integrates_with |
gptkb:Gateway_lunar_station
|
| gptkbp:involved_technology |
gptkb:Advanced_Exploration_Systems
|
| gptkbp:is_a_destination_for |
Moon and Mars
|
| gptkbp:is_a_supporter_of |
public demonstrations of technology
|
| gptkbp:is_capable_of |
supporting crew for 21 days
|
| gptkbp:is_designed_for |
deep space missions
|
| gptkbp:is_explored_in |
Mars missions planned
|
| gptkbp:is_integrated_with |
gptkb:NASA's_Michoud_Assembly_Facility
|
| gptkbp:is_tested_for |
currently in testing
currently in testing phase |
| gptkbp:landing_distance |
gptkb:parachute
splashdown |
| gptkbp:launch_date |
every few years
December 5, 2014 2024 for Artemis II |
| gptkbp:launch_event |
high launch success rate expected
|
| gptkbp:launch_site |
gptkb:Kennedy_Space_Center
gptkb:Cape_Canaveral_Space_Force_Station |
| gptkbp:launch_vehicle |
gptkb:Delta_IV_Heavy
gptkb:Space_Launch_System gptkb:Launch_Complex_39_B gptkb:Space_Launch_System_(SLS) |
| gptkbp:launch_window |
2020s
varies by mission specific launch windows for missions depends on mission |
| gptkbp:length |
5 meters
16.5 feet |
| gptkbp:life_support_system |
gptkb:Environmental_Control_and_Life_Support_System
environmental control and life support system advanced life support system |
| gptkbp:manufacturer |
gptkb:Lockheed_Martin
gptkb:NASA |
| gptkbp:mass |
22,000 kg
|
| gptkbp:media_coverage |
extensive media coverage
|
| gptkbp:mission |
gptkb:2014_Exploration_Flight_Test-1
gptkb:Johnson_Space_Center gptkb:NASA's_Mission_Control_Center gptkb:Artemis_I gptkb:Artemis_II gptkb:Houston,_Texas gptkb:Exploration_Flight_Test-1 gptkb:Artemis_program conducted planned future missions to Mars Artemis III and beyond Lunar orbit and return |
| gptkbp:mission_duration |
up to 30 days
4.5 hours up to 21 days |
| gptkbp:mission_type |
crewed
crewed missions crewed and uncrewed missions |
| gptkbp:movement |
direct reentry
Earth reentry |
| gptkbp:navigation_system |
gptkb:navigation_system
gptkb:Inertial_Navigation_System Inertial navigation system |
| gptkbp:next_uncrewed_mission |
gptkb:Artemis_I
|
| gptkbp:objective |
gptkb:Mars_exploration
return humans to the Moon support human exploration of Mars |
| gptkbp:operational_since |
gptkb:2020
|
| gptkbp:operational_status |
in development
|
| gptkbp:operational_use |
crewed exploration missions
space and reentry |
| gptkbp:orbital_altitude |
Low Earth Orbit
yes up to 1000 km approximately 3,600 miles up to 22,000 miles |
| gptkbp:part_of |
gptkb:NASA's_Artemis_program
|
| gptkbp:partnerships |
collaboration with international space agencies
partnerships with commercial space companies |
| gptkbp:payload_capacity |
up to 10 tons
up to 1,000 kg up to 10,000 kg NASA and contractors |
| gptkbp:power_source |
solar panels
solar energy |
| gptkbp:project |
testing new technologies for Mars missions
project timeline extended due to delays testing future technology for space travel |
| gptkbp:projected_missions |
multiple missions to the Moon and Mars
|
| gptkbp:propulsion |
gptkb:Orion_Service_Module
|
| gptkbp:public_interest |
high
high public interest |
| gptkbp:purpose |
deep space exploration
crew transport transport astronauts crewed lunar missions transport astronauts to lunar orbit crew transport to lunar orbit crewed deep space missions |
| gptkbp:recovery_method |
ocean recovery
ship-based recovery |
| gptkbp:return_speed |
20,000 mph
|
| gptkbp:return_velocity |
25,000 mph
|
| gptkbp:reviews |
conducted engineering reviews regularly
|
| gptkbp:safety_features |
gptkb:launch_escape_system
radiation shielding |
| gptkbp:safety_measures |
multiple
static fire tests stringent safety protocols multiple tests conducted multiple safety tests conducted conducted extensive safety tests various simulations |
| gptkbp:safety_rating |
high
high safety standards high safety rating NASA's safety standards |
| gptkbp:scientific_instruments |
various payloads
various scientific payloads equipped with scientific instruments various instruments for research |
| gptkbp:sensor |
various scientific instruments
multiple sensors for data collection |
| gptkbp:service |
gptkb:European_Space_Agency
|
| gptkbp:spacecraft |
multiple spacecraft systems integrated
|
| gptkbp:speed |
25,000 km/h
25,000 mph approximately 84 degrees up to 40,000 km/h 32,000 km/h |
| gptkbp:successor |
gptkb:spacecraft
|
| gptkbp:support |
21 days
|
| gptkbp:sustainability |
two
reusable components two solar arrays designed for reusability |
| gptkbp:sustainability_efforts |
reduce environmental impact
aligned with sustainability goals of NASA |
| gptkbp:sustainability_features |
reusable components
|
| gptkbp:team |
NASA Recovery Team
NASA recovery team |
| gptkbp:upgrades |
planned future upgrades
planned technology enhancements planned upgrades for Artemis missions |
| gptkbp:used_for |
gptkb:Artemis_missions
crew transport |
| gptkbp:weight |
22,000 pounds
approximately 22,000 pounds around 22,000 pounds |
| gptkbp:width |
4.5 meters
|
| gptkbp:bfsParent |
gptkb:National_Aeronautics_and_Space_Administration
gptkb:NASA |
| gptkbp:bfsLayer |
3
|