|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:combustor_type
|
full-flow staged combustion
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:designed_by
|
gptkb:Space_X
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:diameter
|
1.3 m
|
|
gptkbp:durability
|
reusable
|
|
gptkbp:engine
|
full-flow staged combustion cycle
|
|
gptkbp:engine_configuration
|
two combustion chambers
|
|
gptkbp:engine_type
|
gptkb:Raptor_1
gptkb:Team_Rocket
gptkb:Raptor_2
Raptor Vacuum
Raptor 2.0
|
|
gptkbp:environmental_impact
|
lower than kerosene engines
|
|
gptkbp:first_flight
|
gptkb:Starship_SN20
gptkb:Starship_SN24
gptkb:Starship_SN30
gptkb:Starship_SN40
gptkb:Starship_SN50
gptkb:Starship_SN8
gptkb:Starship_SN1
gptkb:Starship_SN15
gptkb:Starship_SN5
gptkb:2019
Starship SN60
|
|
gptkbp:first_static_fire_test
|
gptkb:2019
|
|
gptkbp:first_test_fire
|
gptkb:2016
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
methane
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Space X Raptor engine
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:intended_use
|
deep space missions
|
|
gptkbp:investment
|
250 bar
|
|
gptkbp:launch_vehicle
|
gptkb:starship
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:number_of_engines
|
gptkb:6
|
|
gptkbp:number_of_engines_in_super_heavy
|
gptkb:33
|
|
gptkbp:number_of_rooms
|
2
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:production_status
|
in development
|
|
gptkbp:propulsion
|
150:1
methane and liquid oxygen
2300 k N
|
|
gptkbp:specific_impulse_sea_level
|
250 s
|
|
gptkbp:specific_impulse_vacuum
|
330 s
|
|
gptkbp:successor
|
gptkb:Merlin_engine
|
|
gptkbp:test_stand_location
|
gptkb:Mc_Gregor,_Texas
|
|
gptkbp:used_in
|
gptkb:starship
|
|
gptkbp:uses
|
methane
liquid oxygen
|
|
gptkbp:weight
|
1,500 kg
|
|
gptkbp:bfsParent
|
gptkb:AR1_rocket_engine
|
|
gptkbp:bfsLayer
|
6
|