Raptor engines

GPTKB entity

Statements (56)
Predicate Object
gptkbp:instance_of gptkb:Team_Rocket
gptkbp:application space launch vehicles
gptkbp:average_temperature -253 to 1500 ° C
gptkbp:collaboration gptkb:NASA
gptkbp:combustion_chamber_pressure 300 bar
gptkbp:cooling_system regenerative cooling
gptkbp:design_purpose high efficiency and reusability
gptkbp:designed_by gptkb:Space_X
gptkbp:development gptkb:2012
gptkbp:development_cost estimated at $1 billion
gptkbp:durability yes
gptkbp:engine full-flow staged combustion
gptkbp:engine_configuration two combustion chambers
gptkbp:engine_type gptkb:Team_Rocket
Raptor 1, Raptor 2
gptkbp:environmental_impact lower than kerosene engines
gptkbp:first_flight gptkb:Starship_SN1
gptkb:2019
2020-05-05
gptkbp:first_static_fire_test 2019-07-24
gptkbp:fuel_capacity 3.1 m
1.3 m
gptkbp:fuel_mass_flow_rate 300 kg/s
gptkbp:fuel_type liquid methane
gptkbp:future_prospects gptkb:Mars_missions
https://www.w3.org/2000/01/rdf-schema#label Raptor engines
gptkbp:ignition_system spark ignition
gptkbp:inspiration gptkb:F-1_engine
gptkbp:investment 250 bar
gptkbp:is_a_supporter_of gptkb:Starship_SN5
gptkbp:is_tested_for gptkb:Space_X_Mc_Gregor
gptkb:Space_X_Boca_Chica
gptkbp:key_feature full-flow staged combustion cycle
gptkbp:launch_cost_reduction aims to reduce costs
gptkbp:launch_vehicle gptkb:starship
gptkbp:max_isp 330 seconds
gptkbp:number_of_engines gptkb:33
gptkb:6
gptkbp:number_of_rooms 2
gptkbp:oxidation_states liquid oxygen
gptkbp:oxidizer_mass_flow_rate 600 kg/s
gptkbp:part_of gptkb:Starship_program
gptkbp:performance better than Merlin engines
gptkbp:production_status in production
gptkbp:project gptkb:Raptor_Vacuum_engine
gptkbp:propulsion 1.5
2300 k N
gptkbp:safety_features multiple redundancies
gptkbp:staged_combustion gptkb:true
gptkbp:successor gptkb:Merlin_engine
gptkbp:used_in gptkb:starship
gptkbp:weight approximately 1,500 kg
gptkbp:bfsParent gptkb:Space_X
gptkb:starship
gptkb:Space_X_Starship
gptkbp:bfsLayer 4