|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
gptkb:Super_Heavy
gptkb:starship
|
|
gptkbp:combustor_type
|
full-flow staged combustion
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:designed_by
|
gptkb:Space_X
|
|
gptkbp:development
|
gptkb:2012
|
|
gptkbp:development_cost
|
estimated at $1 billion
|
|
gptkbp:diameter
|
1.2 m
|
|
gptkbp:durability
|
designed for reuse
|
|
gptkbp:engine_configuration
|
twin-chamber
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
|
gptkbp:facilities
|
gptkb:Space_X_Mc_Gregor
gptkb:Space_X_Boca_Chica
|
|
gptkbp:first_flight
|
gptkb:2020
|
|
gptkbp:first_static_fire
|
gptkb:2019
|
|
gptkbp:first_test_fire
|
gptkb:2019
|
|
gptkbp:fuel_type
|
methane-oxygen
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Raptor engine family
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:investment
|
300 bar
|
|
gptkbp:launch_vehicle
|
gptkb:starship
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:manufacturer
|
gptkb:Space_X
|
|
gptkbp:notable_features
|
high performance
modular design
advanced materials
high reliability
high efficiency
advanced control systems
reusable design
high thrust-to-weight ratio
full-flow staged combustion cycle
environmentally friendly fuel
designed for Mars missions
designed for lunar missions
capable of in-orbit refueling
capable of landing on Mars
capable of landing on the Moon
capable of multiple ignitions
designed for rapid turnaround
high thrust vector control
suitable for deep space missions
|
|
gptkbp:number_of_rooms
|
2
|
|
gptkbp:production_status
|
in production
|
|
gptkbp:propulsion
|
methane
liquid oxygen
2300 k N
|
|
gptkbp:specific_impulse_sea_level
|
250 seconds
|
|
gptkbp:specific_impulse_vacuum
|
330 seconds
|
|
gptkbp:staged_combustion
|
gptkb:true
|
|
gptkbp:successor
|
gptkb:Raptor_2
|
|
gptkbp:uses
|
methane
liquid oxygen
|
|
gptkbp:weight
|
approximately 1,500 kg
|
|
gptkbp:bfsParent
|
gptkb:Raptor_Vacuum_engine
|
|
gptkbp:bfsLayer
|
6
|