|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
launch vehicles
|
|
gptkbp:check_in_time
|
150 seconds
|
|
gptkbp:collaboration
|
with various space agencies
|
|
gptkbp:combustor_type
|
staged combustion
|
|
gptkbp:contribution
|
to propulsion technology
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:cultural_impact
|
featured in documentaries
|
|
gptkbp:debut
|
multiple successful launches
|
|
gptkbp:design
|
gptkb:Oleg_Kuznetsov
|
|
gptkbp:design_date
|
1960s
|
|
gptkbp:development
|
gptkb:Soviet_Union
|
|
gptkbp:development_cost
|
high
|
|
gptkbp:difficulty
|
high
|
|
gptkbp:educational_use
|
in engineering programs
|
|
gptkbp:engine
|
staged combustion cycle
|
|
gptkbp:engine_configuration
|
vertical
|
|
gptkbp:environmental_impact
|
low emissions
|
|
gptkbp:exhaust_system
|
bell nozzle
|
|
gptkbp:first_flight
|
gptkb:1987
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
requires special handling
kerosene
|
|
gptkbp:has_documentation
|
extensive records available
|
|
gptkbp:historical_significance
|
pioneered multi-chamber designs
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-170 engine
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:influence
|
on future rocket designs
|
|
gptkbp:inspired
|
gptkb:RD-180_engine
|
|
gptkbp:invention
|
held by Kuznetsov
|
|
gptkbp:is_tested_for
|
extensive
Kuznetsov's test facility
|
|
gptkbp:legacy
|
influenced modern rocket engines
|
|
gptkbp:manufacturer
|
gptkb:Kuznetsov
|
|
gptkbp:material
|
advanced alloys
|
|
gptkbp:notable_feature
|
four combustion chambers
|
|
gptkbp:number_of_rooms
|
four
25 MPa
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:operational_use
|
1990s
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:oxidizer_storage
|
requires special handling
|
|
gptkbp:performance
|
excellent
|
|
gptkbp:produces
|
over 100
|
|
gptkbp:propulsion
|
1.42
RP-1 and LOX
1700 k N
|
|
gptkbp:public_displays
|
in museums
|
|
gptkbp:reliability
|
high
|
|
gptkbp:retirement_year
|
2000s
|
|
gptkbp:safety_features
|
multiple redundancies
|
|
gptkbp:specific_impulse
|
311 s
|
|
gptkbp:successor
|
gptkb:RD-180_engine
|
|
gptkbp:used_by
|
gptkb:Ukrainian_Space_Agency
|
|
gptkbp:used_in
|
gptkb:Zenit_rocket
|
|
gptkbp:water_requirement
|
300 kg/s
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Energia_launch_vehicle
|
|
gptkbp:bfsLayer
|
5
|