|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:application
|
space launch vehicles
|
|
gptkbp:controls
|
gptkb:electronic
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:debut_year
|
limited
|
|
gptkbp:design
|
modular design
Kuznetsov team
|
|
gptkbp:developer
|
gptkb:unknown
1960s
|
|
gptkbp:engine
|
excellent
spark ignition
|
|
gptkbp:engine_type
|
gptkb:none
gptkb:rocket
|
|
gptkbp:environmental_impact
|
moderate
|
|
gptkbp:facilities
|
gptkb:Kuznetsov_Design_Bureau
|
|
gptkbp:first_flight
|
gptkb:1965
multiple
|
|
gptkbp:fuel_capacity
|
gptkb:unknown
4.5 m
1.5 m
high
|
|
gptkbp:fuel_type
|
staged combustion
kerosene
turbopump
|
|
gptkbp:has_documentation
|
gptkb:stock_market_index
|
|
gptkbp:historical_significance
|
first engine to use staged combustion in the USSR
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-170
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:innovation
|
high thrust-to-weight ratio
|
|
gptkbp:inspiration
|
gptkb:RD-180_engine
|
|
gptkbp:invention
|
multiple
|
|
gptkbp:launch_vehicle
|
N-1
|
|
gptkbp:legacy
|
influenced modern rocket engines
|
|
gptkbp:manufacturer
|
gptkb:Kuznetsov
|
|
gptkbp:material
|
aluminum alloys
|
|
gptkbp:notable_feature
|
four combustion chambers
|
|
gptkbp:notable_users
|
gptkb:Soviet_space_program
|
|
gptkbp:number_of_rooms
|
four
|
|
gptkbp:number_of_stages
|
single stage
|
|
gptkbp:operational_area
|
gptkb:Soviet_space_missions
1965-1974
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:propulsion
|
2.13
1700 k N
|
|
gptkbp:rate_of_fire
|
3200 K
150 seconds
|
|
gptkbp:reliability
|
high
|
|
gptkbp:research_areas
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:social_structure
|
liquid oxygen
|
|
gptkbp:successor
|
gptkb:RD-180
|
|
gptkbp:tail_type
|
converging-diverging
|
|
gptkbp:trigger_type
|
300 s
|
|
gptkbp:used_in
|
gptkb:N-1_rocket
|
|
gptkbp:valve_configuration
|
25 M Pa
|
|
gptkbp:weight
|
800 kg
|
|
gptkbp:bfsParent
|
gptkb:Energia
|
|
gptkbp:bfsLayer
|
4
|