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gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
gptkb:Space_Launch_System
|
|
gptkbp:check_in_time
|
150 seconds
|
|
gptkbp:combustor_type
|
staged combustion
|
|
gptkbp:control_system
|
digital
|
|
gptkbp:cooling_system
|
regenerative cooling
regenerative cooling system
|
|
gptkbp:designed_by
|
gptkb:Kuznetsov
|
|
gptkbp:development
|
gptkb:Soviet_Union
1970s to 1980s
|
|
gptkbp:engine
|
gptkb:space_exploration
gptkb:Kuznetsov
influenced future designs
staged combustion cycle
part of Soviet space history
ongoing research into improvements
|
|
gptkbp:engine_configuration
|
vertical
clustered
detailed specifications available
|
|
gptkbp:engine_power
|
high performance
high reliability
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
various variants developed.
|
|
gptkbp:exhaust_system
|
bell nozzle
|
|
gptkbp:first_flight
|
gptkb:1987
|
|
gptkbp:fuel_capacity
|
2.5 m
4.5 m
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-0120 engine
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:launched
|
Energia missions
|
|
gptkbp:number_of_rooms
|
four
single combustion chamber
20 MPa
|
|
gptkbp:operational_use
|
launching payloads
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:propulsion
|
yes
1800 k N
|
|
gptkbp:related_to
|
gptkb:Soviet_space_program
|
|
gptkbp:specific_impulse
|
300 seconds
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
RD-0124 engine
|
|
gptkbp:type
|
liquid-fueled
|
|
gptkbp:used_in
|
gptkb:Energia_rocket
|
|
gptkbp:water_requirement
|
100 kg/s
200 kg/s
|
|
gptkbp:weight
|
3000 kg
|
|
gptkbp:bfsParent
|
gptkb:Energia_launch_vehicle
|
|
gptkbp:bfsLayer
|
5
|