|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
launch vehicles
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:check_in_time
|
approximately 150 seconds
|
|
gptkbp:combustor_type
|
staged combustion
|
|
gptkbp:control_system
|
digital
|
|
gptkbp:cooling_system
|
efficient
regenerative cooling
|
|
gptkbp:designed_by
|
gptkb:Kuznetsov
|
|
gptkbp:development
|
ongoing
|
|
gptkbp:development_cost
|
classified
|
|
gptkbp:engine
|
ongoing
advanced
successful
satellite launches
documented
staged combustion cycle
|
|
gptkbp:engine_configuration
|
available
modern
vertical
|
|
gptkbp:engine_development_phase
|
completed
|
|
gptkbp:engine_ignition_method
|
reliable
|
|
gptkbp:engine_power
|
high
long
high efficiency
documented
optimized
|
|
gptkbp:engine_testing_results
|
positive
|
|
gptkbp:engine_type
|
gptkb:RD-191
|
|
gptkbp:environment
|
gptkb:space
|
|
gptkbp:facilities
|
Kuznetsov test site
|
|
gptkbp:first_flight
|
gptkb:2014
|
|
gptkbp:fuel_type
|
kerosene
turbopump
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-190 engine
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:is_tested_for
|
gptkb:Kuznetsov
completed
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
Angara family
|
|
gptkbp:manufacturer
|
Russian space industry
|
|
gptkbp:number_of_rooms
|
four
approximately 100 bar
|
|
gptkbp:operational_status
|
in use
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:propulsion
|
yes
high
enabled
RP-1 and LOX
190 k N
190 k N at sea level
|
|
gptkbp:specific_impulse
|
300 seconds
|
|
gptkbp:successor
|
gptkb:RD-191_engine
|
|
gptkbp:type
|
liquid-fueled
|
|
gptkbp:used_in
|
gptkb:Angara_rocket
|
|
gptkbp:weight
|
approximately 600 kg
|
|
gptkbp:bfsParent
|
gptkb:RD-600_engine
|
|
gptkbp:bfsLayer
|
8
|