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gptkbp:instance_of
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gptkb:spacecraft
|
|
gptkbp:academic_programs
|
Experienced engineers
|
|
gptkbp:advances
|
Next-gen propulsion
|
|
gptkbp:air_traffic_control
|
Fly-by-wire system
|
|
gptkbp:aircraft_operated
|
Low Earth Orbit
Variable
|
|
gptkbp:budget
|
$2 billion
|
|
gptkbp:cargo_capacity
|
100 tons to LEO
|
|
gptkbp:challenges
|
Heat shield development
|
|
gptkbp:collaboration
|
gptkb:NASA
Global partnerships
|
|
gptkbp:community_engagement
|
Public events
|
|
gptkbp:control_system
|
Autonomous landing system
|
|
gptkbp:crew
|
Ongoing
|
|
gptkbp:crew_capacity
|
gptkb:100
|
|
gptkbp:design
|
Continuous
Ongoing
Modular design
Space X engineers
|
|
gptkbp:design_features
|
Aerodynamic shape
|
|
gptkbp:design_purpose
|
Interplanetary travel
|
|
gptkbp:designed_by
|
gptkb:Space_X
|
|
gptkbp:development
|
Aggressive
|
|
gptkbp:diameter
|
9 meters
|
|
gptkbp:durability
|
Fully reusable
|
|
gptkbp:engineering_milestones
|
Completed prototypes
|
|
gptkbp:environmental_impact
|
Low emissions
|
|
gptkbp:first_flight
|
gptkb:2023
gptkb:Texas
Planned
Validate systems
|
|
gptkbp:fuel_type
|
Liquid methane and liquid oxygen
|
|
gptkbp:future_plans
|
Mars colonization
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Starship Mk32
|
|
gptkbp:innovation
|
Safety and reliability
|
|
gptkbp:inspiration
|
gptkb:Starship_Mk1
gptkb:science_fiction
|
|
gptkbp:is_a_destination_for
|
gptkb:Mars
|
|
gptkbp:is_tested_for
|
Static fire test
|
|
gptkbp:landing_distance
|
Vertical landing
|
|
gptkbp:launch_date
|
2025
Frequent
|
|
gptkbp:launch_mass
|
1200 tons
|
|
gptkbp:launch_platform
|
gptkb:Space_X
|
|
gptkbp:launch_site
|
gptkb:Space_X_Starbase
|
|
gptkbp:launch_vehicle
|
gptkb:Super_Heavy_booster
|
|
gptkbp:launch_window
|
Open-ended
|
|
gptkbp:length
|
50 meters
|
|
gptkbp:manufacturer
|
gptkb:Space_X
|
|
gptkbp:material
|
Stainless steel
|
|
gptkbp:media_coverage
|
Extensive
|
|
gptkbp:mission
|
Lunar landings
|
|
gptkbp:number_of_engines
|
gptkb:6
|
|
gptkbp:operational_use
|
Commercial missions
|
|
gptkbp:orbital_altitude
|
7.8 km/s
|
|
gptkbp:payload_capacity
|
100 tons
Integrated
150 tons to LEO
|
|
gptkbp:production_status
|
gptkb:prototype
|
|
gptkbp:project
|
In-situ resource utilization
|
|
gptkbp:propulsion
|
gptkb:Raptor_engines
2300 k N
|
|
gptkbp:public_interest
|
gptkb:High
|
|
gptkbp:public_reveal
|
gptkb:2022
|
|
gptkbp:purpose
|
gptkb:Space_exploration
|
|
gptkbp:recovery_method
|
Landing on drone ship
|
|
gptkbp:safety_features
|
gptkb:launch_escape_system
|
|
gptkbp:status
|
In development
|
|
gptkbp:support
|
gptkb:Strong
|
|
gptkbp:sustainability_efforts
|
Reduce space debris
|
|
gptkbp:test_flight_frequency
|
gptkb:Regular
|
|
gptkbp:bfsParent
|
gptkb:Starship_SN14
|
|
gptkbp:bfsLayer
|
5
|