|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
space launch vehicles
|
|
gptkbp:combustion_chamber_pressure
|
250 bar
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:cycle_type
|
full-flow staged combustion
|
|
gptkbp:design_purpose
|
reusability
|
|
gptkbp:development
|
gptkb:2012
Space X engineers
|
|
gptkbp:engine_configuration
|
dual combustion chamber
|
|
gptkbp:engine_type
|
gptkb:Raptor_1
gptkb:Team_Rocket
gptkb:Raptor_2
Raptor Vacuum
|
|
gptkbp:environmental_impact
|
lower than kerosene engines
|
|
gptkbp:first_flight
|
gptkb:2019
|
|
gptkbp:first_static_fire_test
|
gptkb:2019
|
|
gptkbp:fuel_capacity
|
3.5 m
1.3 m
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
liquid methane
|
|
gptkbp:future_prospects
|
gptkb:Mars_missions
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Raptor rocket engine
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:innovation
|
advanced materials
|
|
gptkbp:integration
|
integrated with Starship
|
|
gptkbp:investment
|
high pressure
|
|
gptkbp:is_tested_for
|
gptkb:Space_X_Mc_Gregor
ongoing
extensive testing
|
|
gptkbp:launch_date
|
high frequency
|
|
gptkbp:launch_vehicle
|
gptkb:starship
|
|
gptkbp:manufacturer
|
gptkb:Space_X
|
|
gptkbp:notable_feature
|
full-flow staged combustion cycle
|
|
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:performance
|
high performance
|
|
gptkbp:production_status
|
in development
|
|
gptkbp:project
|
improved versions
|
|
gptkbp:propulsion
|
methane and oxygen
2300 k N
~150:1
|
|
gptkbp:reusability_goal
|
multiple flights
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:specific_impulse
|
330 seconds (sea level)
|
|
gptkbp:specific_impulse_vacuum
|
330 seconds (vacuum)
|
|
gptkbp:successor
|
gptkb:Merlin_engine
|
|
gptkbp:used_in
|
gptkb:starship
|
|
gptkbp:weight
|
1,500 kg
|
|
gptkbp:bfsParent
|
gptkb:NASA's_Stennis_Space_Center
|
|
gptkbp:bfsLayer
|
5
|