|
gptkbp:instanceOf
|
space launch system
|
|
gptkbp:budget
|
$18 billion
|
|
gptkbp:crewCapacity
|
4 to 6 astronauts
|
|
gptkbp:design
|
gptkb:Lockheed_Martin
gptkb:Northrop_Grumman
gptkb:Boeing
Aerojet Rocketdyne
flexible
modular
evolvable
|
|
gptkbp:developedBy
|
NASA
|
|
gptkbp:engineType
|
RS-25
Solid rocket boosters
|
|
gptkbp:firstFlight
|
2021
Artemis I
Green Run
|
|
gptkbp:funding
|
NASA_budget
|
|
gptkbp:futurePlans
|
gptkb:Lunar_Gateway
Artemis II
Artemis III
Mars_missions
Asteroid_missions
|
|
gptkbp:goal
|
return humans to the Moon
send_humans_to_Mars
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
NASA's Space Launch System program
|
|
gptkbp:internationalCooperation
|
gptkb:JAXA
gptkb:ESA
CSA
|
|
gptkbp:launched
|
1-2 missions per year
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:launchVehicle
|
gptkb:SLS_Block_1
gptkb:SLS_Block_2
gptkb:SLS_Block_1B
|
|
gptkbp:lifespan
|
20 years
multiple missions
|
|
gptkbp:payloadCapacity
|
130 metric tons to LEO (Block 2)
95 metric tons to LEO
|
|
gptkbp:productionCompany
|
2011
|
|
gptkbp:publicAccess
|
high
|
|
gptkbp:purpose
|
deep space exploration
|
|
gptkbp:relatedPatent
|
gptkb:Artemis_program
|
|
gptkbp:replacedBy
|
Space Shuttle
|
|
gptkbp:safetyFeatures
|
redundant systems
abort system
|
|
gptkbp:secondaryMission
|
Artemis I
|