|
gptkbp:instanceOf
|
rocket
|
|
gptkbp:applicationStatus
|
active
|
|
gptkbp:controls
|
digital fly-by-wire
|
|
gptkbp:crewCapacity
|
gptkb:Orion_spacecraft
4 astronauts
|
|
gptkbp:designedBy
|
NASA
|
|
gptkbp:developer
|
$18 billion
|
|
gptkbp:diameter
|
8.4 meters
|
|
gptkbp:enginePower
|
1,000,000 pounds of thrust per engine
|
|
gptkbp:engineType
|
liquid-fueled
|
|
gptkbp:firstAwarded
|
RS-25 engines
|
|
gptkbp:firstFlight
|
2021
Green Run
Artemis_I_launch
|
|
gptkbp:fuelType
|
liquid hydrogen and liquid oxygen
|
|
gptkbp:futurePlans
|
gptkb:Lunar_Gateway
sample return missions
interplanetary missions
Mars_missions
human_exploration_of_Mars
|
|
gptkbp:hasArea
|
gptkb:NASA_Stennis_Space_Center
gptkb:NASA_Michoud_Assembly_Facility
|
|
gptkbp:hasGoals
|
two
|
|
gptkbp:height
|
98 meters
|
|
gptkbp:homeGround
|
mobile launcher
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
The Space Launch System
|
|
gptkbp:internationalCooperation
|
gptkb:Canadian_Space_Agency
gptkb:European_Space_Agency
gptkb:Japanese_Aerospace_Exploration_Agency
|
|
gptkbp:launched
|
$2 billion per launch
once every 2-3 years
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
gptkb:Northrop_Grumman
gptkb:Boeing
Aerojet Rocketdyne
|
|
gptkbp:mission
|
gptkb:Moon
gptkb:Mars
Asteroids
|
|
gptkbp:payloadCapacity
|
up to 130 tons
|
|
gptkbp:productionCompany
|
2011
|
|
gptkbp:project
|
2025
|
|
gptkbp:propulsion
|
8.8 million pounds
|
|
gptkbp:publicAccess
|
high
|
|
gptkbp:purpose
|
deep space exploration
|
|
gptkbp:relatedPatent
|
gptkb:Artemis_program
Artemis I
Artemis II
Artemis III
Exploration Mission-1
|
|
gptkbp:reliability
|
not_reusable
|
|
gptkbp:safetyFeatures
|
multiple redundant systems
|