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gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:air_traffic_control
|
Fly-by-wire system
|
|
gptkbp:cargo_capacity
|
up to 100 metric tons to LEO
|
|
gptkbp:category
|
gptkb:Space_Launch_System
|
|
gptkbp:challenges
|
Thermal protection
|
|
gptkbp:collaboration
|
gptkb:NASA
|
|
gptkbp:community_engagement
|
Public outreach programs
|
|
gptkbp:community_support
|
Strong support from space enthusiasts
|
|
gptkbp:control_system
|
Autonomous landing system
|
|
gptkbp:cooling_system
|
Ablative heat shield
|
|
gptkbp:crew_capacity
|
up to 100 people
|
|
gptkbp:debut
|
TBD
|
|
gptkbp:design
|
Modular design
Space X engineers
|
|
gptkbp:design_features
|
Aerodynamic shape
|
|
gptkbp:design_purpose
|
Interplanetary travel
|
|
gptkbp:designed_by
|
gptkb:Space_X
|
|
gptkbp:development
|
Ongoing
|
|
gptkbp:diameter
|
9 meters
|
|
gptkbp:durability
|
Fully reusable
|
|
gptkbp:environmental_impact
|
Designed for minimal impact
|
|
gptkbp:first_flight
|
gptkb:2023
Planned for 2024
|
|
gptkbp:fuel_type
|
Liquid methane and liquid oxygen
|
|
gptkbp:future_prospects
|
Tourism and colonization
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Starship Mk31
|
|
gptkbp:innovation
|
Safety and efficiency
|
|
gptkbp:inspiration
|
gptkb:Starship_Mk1
gptkb:science_fiction
|
|
gptkbp:is_a_destination_for
|
gptkb:Mars
|
|
gptkbp:is_a_supporter_of
|
Planned for 2024
|
|
gptkbp:is_tested_for
|
gptkb:Boca_Chica,_Texas
Prototype testing
Static fire test
|
|
gptkbp:landing_distance
|
Vertical landing
|
|
gptkbp:launch_date
|
2025
Multiple launches per year
|
|
gptkbp:launch_mass
|
200 metric tons
|
|
gptkbp:launch_price
|
Estimated $2 million per launch
|
|
gptkbp:launch_site
|
gptkb:Space_X_Starbase
|
|
gptkbp:length
|
50 meters
|
|
gptkbp:manufacturer
|
gptkb:Space_X
|
|
gptkbp:mission
|
Lunar landings
Earth to Mars
|
|
gptkbp:number_of_engines
|
6 Raptor engines
|
|
gptkbp:operational_range
|
Low Earth Orbit to Mars
|
|
gptkbp:orbital_altitude
|
7.8 km/s
|
|
gptkbp:partnerships
|
International space agencies
|
|
gptkbp:payload_capacity
|
100 metric tons
No fairing required
|
|
gptkbp:project
|
In-situ resource utilization
Human settlement on Mars
|
|
gptkbp:propulsion
|
gptkb:Raptor_engines
|
|
gptkbp:public_interest
|
gptkb:High
|
|
gptkbp:public_reveal
|
gptkb:2022
|
|
gptkbp:purpose
|
gptkb:Space_exploration
|
|
gptkbp:safety_features
|
Multiple redundancy systems
|
|
gptkbp:specification
|
Advanced avionics
|
|
gptkbp:status
|
In development
|
|
gptkbp:sustainability
|
Reusable components
|
|
gptkbp:weight
|
120 metric tons
|
|
gptkbp:bfsParent
|
gptkb:Starship_SN14
|
|
gptkbp:bfsLayer
|
5
|