|
gptkbp:instance_of
|
gptkb:Ariane_5
|
|
gptkbp:collaboration
|
gptkb:Artemis_program
|
|
gptkbp:configuration
|
gptkb:block_1_B
gptkb:block_2
block 1
|
|
gptkbp:crew_capacity
|
up to 4 astronauts
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:development
|
gptkb:2011
|
|
gptkbp:development_cost
|
$18 billion
|
|
gptkbp:diameter
|
8.4 meters
|
|
gptkbp:durability
|
not reusable
|
|
gptkbp:engine_type
|
gptkb:RS-25
|
|
gptkbp:first_flight
|
gptkb:2021
uncrewed test flight
|
|
gptkbp:future_plans
|
gptkb:Artemis_Moon_landings
gptkb:Lunar_Gateway
gptkb:Mars_missions
Interplanetary missions
Asteroid missions
|
|
gptkbp:has_programs
|
active
|
|
gptkbp:height
|
98 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Space Launch System family
|
|
gptkbp:inspiration
|
gptkb:Constellation_program
gptkb:Apollo_program
gptkb:Space_Shuttle
|
|
gptkbp:launch_date
|
1-2 launches per year
|
|
gptkbp:launch_price
|
$2 billion per launch
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
heavy-lift launch vehicle
two solid rocket boosters
|
|
gptkbp:manufacturer
|
gptkb:Aerojet_Rocketdyne
gptkb:Lockheed_Martin
gptkb:Northrop_Grumman
gptkb:Boeing
gptkb:NASA
|
|
gptkbp:mission
|
gptkb:Johnson_Space_Center
|
|
gptkbp:number_of_engines
|
gptkb:4
|
|
gptkbp:number_of_stages
|
ICPS
core stage
|
|
gptkbp:orbital_altitude
|
28,000 km/h
|
|
gptkbp:payload_capacity
|
95 metric tons to LEO
|
|
gptkbp:purpose
|
deep space exploration
|
|
gptkbp:safety_rating
|
high
|
|
gptkbp:successor
|
gptkb:Space_Shuttle
|
|
gptkbp:targets
|
gptkb:Artemis_I
gptkb:Artemis_II
gptkb:Artemis_III
|
|
gptkbp:bfsParent
|
gptkb:Space_Launch_Systems
gptkb:NASA's_Space_Launch_System_(SLS)
|
|
gptkbp:bfsLayer
|
5
|