|
gptkbp:instanceOf
|
gptkb:spacecraft
|
|
gptkbp:averageRainfall
|
$2 billion per launch
|
|
gptkbp:built
|
Thermal protection system
|
|
gptkbp:collaborations
|
gptkb:ESA
|
|
gptkbp:communicationEquipment
|
S-band and Ku-band
|
|
gptkbp:community_engagement
|
High
Educational outreach programs
|
|
gptkbp:crew
|
NASA astronauts
NASA Astronaut Corps
|
|
gptkbp:crew_size
|
4 astronauts
|
|
gptkbp:criteria
|
Weather and technical readiness
|
|
gptkbp:design
|
15 years
|
|
gptkbp:electronicSystems
|
NASA_engineers
|
|
gptkbp:engineConfiguration
|
Aerojet Rocketdyne
|
|
gptkbp:engineType
|
RS-25
|
|
gptkbp:environmental_impact
|
Minimized emissions
|
|
gptkbp:firstFlight
|
2028
|
|
gptkbp:fuelType
|
Liquid hydrogen and liquid oxygen
|
|
gptkbp:future_plans
|
Green Run
|
|
gptkbp:height
|
98 meters
|
|
gptkbp:historical_significance
|
Part_of_NASA's_return_to_the_Moon
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SLS Block 4
|
|
gptkbp:is_integrated_with
|
Orion_and_Gateway
|
|
gptkbp:launchDate
|
1 every 2 years
|
|
gptkbp:launched
|
4
Open-ended
Vertical integration
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launchVehicle
|
Advanced propulsion systems
Heavy-lift launch vehicle
Translunar_injection
|
|
gptkbp:leads
|
gptkb:John_Honeycutt
|
|
gptkbp:lifespan
|
20 missions
|
|
gptkbp:manufacturer
|
NASA
|
|
gptkbp:mission
|
Crewed and uncrewed missions
|
|
gptkbp:missions
|
gptkb:Johnson_Space_Center
Mars_missions
|
|
gptkbp:number_of_stages
|
4
ICPS
|
|
gptkbp:orbitalInclination
|
Lunar orbit
Delta-v calculations
|
|
gptkbp:passenger_traffic
|
130 metric tons
|
|
gptkbp:payloadCapacity
|
gptkb:Lunar_Gateway
|
|
gptkbp:produces
|
2019
|
|
gptkbp:project
|
Agile methodology
|
|
gptkbp:propulsion
|
2,000,000 pounds
|
|
gptkbp:provides
|
Inertial navigation system
|
|
gptkbp:purpose
|
Deep space exploration
|
|
gptkbp:relatedPatent
|
gptkb:Artemis_program
|
|
gptkbp:reliability
|
No
|
|
gptkbp:revenue
|
$10 billion
|
|
gptkbp:riskManagement
|
Comprehensive risk assessment
|
|
gptkbp:safety_features
|
Launch escape system
|
|
gptkbp:safetyFeatures
|
NASA_safety_protocols
|
|
gptkbp:secondary_mission
|
gptkb:Orion_spacecraft
|
|
gptkbp:stakeholders
|
NASA,_contractors,_and_international_partners
|
|
gptkbp:successor
|
gptkb:SLS_Block_1
|
|
gptkbp:supplyChain
|
Multiple contractors
|
|
gptkbp:tourism
|
30 days
|
|
gptkbp:training
|
Mobile launcher
|