|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:academic_programs
|
Space X engineers
|
|
gptkbp:aircraft_operated
|
10 km
6 minutes
Approximately 10 minutes
approximately 6 minutes
|
|
gptkbp:budget
|
estimated $2 billion
|
|
gptkbp:challenges
|
thermal protection system
Overcome during development
|
|
gptkbp:collaboration
|
gptkb:NASA
|
|
gptkbp:community_engagement
|
local outreach programs
Involved local community
|
|
gptkbp:control_system
|
autonomous landing system
Autonomous flight control
|
|
gptkbp:crew
|
gptkb:None
|
|
gptkbp:crew_capacity
|
gptkb:0
up to 100
|
|
gptkbp:design
|
Space X engineers
|
|
gptkbp:design_features
|
Stainless steel structure
|
|
gptkbp:design_purpose
|
Interplanetary travel
interplanetary travel
|
|
gptkbp:diameter
|
9 meters
9 m
|
|
gptkbp:durability
|
fully reusable
|
|
gptkbp:elevation
|
10 km
|
|
gptkbp:engine_type
|
gptkb:Raptor_engine
gptkb:Raptor_engines
|
|
gptkbp:environmental_impact
|
low emissions
Considered in design
|
|
gptkbp:first_flight
|
gptkb:Starship_SN18
gptkb:17
gptkb:Boca_Chica,_Texas
gptkb:Yes
2021-12-09
Suborbital
partial success
High-altitude flight
April 20, 2022
SN17
Post-flight analysis conducted
exploded on landing
Validate design and performance
Advancement of reusable spacecraft technology
Conducted prior to launch
Explosive disassembly
Telemetry collected
second test flight
|
|
gptkbp:flight_style
|
suborbital
Vertical ascent and descent
|
|
gptkbp:fuel_type
|
Liquid methane and liquid oxygen
liquid methane and liquid oxygen
|
|
gptkbp:future_plans
|
Further testing and development
|
|
gptkbp:height
|
50 m
50 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Starship SN17
|
|
gptkbp:influenced_by
|
gptkb:Starship_SN8
|
|
gptkbp:inspiration
|
gptkb:Starship_SN1
Mars colonization
|
|
gptkbp:involved_in
|
gptkb:NASA_Artemis_program
|
|
gptkbp:involved_technology
|
gptkb:Starship_SN_series
|
|
gptkbp:is_a_supporter_of
|
gptkb:Yes
|
|
gptkbp:is_tested_for
|
high-altitude flight
|
|
gptkbp:landing_distance
|
belly flop
Ocean landing
|
|
gptkbp:launch_date
|
2022-04-20
2021-12-09
15:00 UTC
|
|
gptkbp:launch_event
|
Failure
Publicly attended
|
|
gptkbp:launch_mass
|
300000 kg
|
|
gptkbp:launch_platform
|
gptkb:Space_X
|
|
gptkbp:launch_site
|
gptkb:Space_X_Boca_Chica
|
|
gptkbp:launch_window
|
gptkb:2021
|
|
gptkbp:launched
|
Extensive testing prior to flight
|
|
gptkbp:manufacturer
|
gptkb:Space_X
|
|
gptkbp:mass
|
120000 kg
|
|
gptkbp:media_coverage
|
Extensive
extensive
|
|
gptkbp:mission
|
aerodynamic testing
Orbital flight test
|
|
gptkbp:mission_type
|
Test flight
|
|
gptkbp:number_of_engines
|
gptkb:3
gptkb:6
|
|
gptkbp:number_of_stages
|
gptkb:Super_Heavy_booster
|
|
gptkbp:operational_status
|
Not operational
|
|
gptkbp:operational_use
|
future missions
|
|
gptkbp:part_of
|
gptkb:Starship_program
|
|
gptkbp:payload_capacity
|
100 metric tons
100 tons to LEO
|
|
gptkbp:predecessor
|
gptkb:Starship_SN16
|
|
gptkbp:production_status
|
gptkb:prototype
|
|
gptkbp:project
|
ongoing
Prototype testing
|
|
gptkbp:propulsion
|
2300 k N
|
|
gptkbp:public_interest
|
gptkb:High
high
|
|
gptkbp:related_to
|
gptkb:Starship_SN16
gptkb:Starship_SN15
Mars colonization
|
|
gptkbp:related_vehicle
|
Reusable launch system
|
|
gptkbp:safety_features
|
multiple redundancy systems
|
|
gptkbp:safety_measures
|
Implemented during testing
|
|
gptkbp:specification
|
Documented in engineering reports
|
|
gptkbp:status
|
destroyed
Destroyed
|
|
gptkbp:success
|
False
|
|
gptkbp:successor
|
gptkb:Starship_SN18
gptkb:Starship_SN20
|
|
gptkbp:test_flight_number
|
SN17
|
|
gptkbp:test_flight_outcome_details
|
exploded during landing attempt.
|
|
gptkbp:bfsParent
|
gptkb:Space_X's_Starship_program
|
|
gptkbp:bfsLayer
|
4
|