gptkbp:instance_of
|
gptkb:Team_Rocket
|
gptkbp:average_temperature
|
-253 ° C to 1,000 ° C
|
gptkbp:collaboration
|
gptkb:NASA
|
gptkbp:control_system
|
digital control system
|
gptkbp:cooling_system
|
regenerative cooling
|
gptkbp:cycle_type
|
full-flow staged combustion
|
gptkbp:design_purpose
|
interplanetary travel
|
gptkbp:designed_by
|
gptkb:Space_X
|
gptkbp:development_cost
|
estimated at $1 billion
|
gptkbp:durability
|
reusable
|
gptkbp:engine
|
extensive research conducted
ongoing development
various space missions
innovative design features
|
gptkbp:engine_community_feedback
|
feedback from aerospace community
|
gptkbp:engine_configuration
|
detailed specifications available
clustered configuration
|
gptkbp:engine_future_plans
|
future plans for upgrades
|
gptkbp:engine_launch_count
|
multiple launches
|
gptkbp:engine_power
|
high efficiency
performance metrics tracked
|
gptkbp:engine_type
|
gptkb:Team_Rocket
Raptor 1, Raptor 2
|
gptkbp:exhaust_system
|
aerospike nozzle
|
gptkbp:first_flight
|
gptkb:2019
|
gptkbp:fuel_capacity
|
3.5 m
1.3 m
|
gptkbp:fuel_type
|
liquid methane
|
gptkbp:future_prospects
|
gptkb:Mars_missions
|
https://www.w3.org/2000/01/rdf-schema#label
|
Starship Raptor engines
|
gptkbp:ignition_system
|
spark ignition
|
gptkbp:inspiration
|
gptkb:F-1_engine
|
gptkbp:is_tested_for
|
gptkb:Mc_Gregor_test_facility
gptkb:Space_X_Boca_Chica
static fire testing
ongoing testing
|
gptkbp:launch_vehicle
|
Starship launch vehicle
|
gptkbp:max_isp
|
330 seconds
|
gptkbp:number_of_engines
|
up to 6
|
gptkbp:number_of_rooms
|
single combustion chamber
250 bar
|
gptkbp:oxidation_states
|
liquid oxygen
|
gptkbp:part_of
|
gptkb:Starship_program
|
gptkbp:performance
|
high performance
|
gptkbp:production_status
|
in development
|
gptkbp:propellant_mass_flow_rate
|
300 kg/s
|
gptkbp:propulsion
|
1.53
2300 k N
|
gptkbp:sustainability
|
designed for sustainability
|
gptkbp:used_in
|
gptkb:Starship_spacecraft
|
gptkbp:weight
|
approximately 1,500 kg
|
gptkbp:bfsParent
|
gptkb:Starship_SN2
|
gptkbp:bfsLayer
|
6
|