|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:BE-4
|
|
gptkbp:application
|
interplanetary travel
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:design
|
reusability
|
|
gptkbp:developer
|
gptkb:2012
|
|
gptkbp:durability
|
gptkb:battle
|
|
gptkbp:engine
|
gptkb:advanced_technology
gptkb:33
gptkb:6
high
multiple
ongoing
deep space missions
optimized for efficiency
single nozzle
full-flow staged combustion cycle
new propulsion technology
|
|
gptkbp:engine_type
|
gptkb:Raptor_1
gptkb:Raptor_2
full-flow staged combustion
Raptor Vacuum
|
|
gptkbp:first_flight
|
gptkb:2019
gptkb:2020
|
|
gptkbp:fuel_capacity
|
1.3 m
250 bar
|
|
gptkbp:fuel_type
|
liquid methane
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Space X Raptor
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:is_tested_for
|
gptkb:Space_X_Mc_Gregor
gptkb:Mc_Gregor,_Texas
gptkb:Space_X_Boca_Chica
static fire tests
|
|
gptkbp:launch_vehicle
|
gptkb:starship
|
|
gptkbp:manufacturer
|
gptkb:Space_X
|
|
gptkbp:operational_area
|
Starship missions
|
|
gptkbp:produced_by
|
in production
|
|
gptkbp:propulsion
|
methane and oxygen
1.53
2300 k N
2300 k N (sea level)
2600 k N (vacuum)
3100 k N
330 seconds (sea level)
330 seconds (vacuum)
350 seconds (vacuum)
|
|
gptkbp:rate_of_fire
|
gptkb:2019
|
|
gptkbp:reliability
|
high
|
|
gptkbp:social_structure
|
liquid oxygen
|
|
gptkbp:successor
|
gptkb:Merlin_engine
|
|
gptkbp:used_in
|
gptkb:starship
|
|
gptkbp:weight
|
1,500 kg
|