RD-0110 engines

GPTKB entity

Statements (51)
Predicate Object
gptkbp:instance_of gptkb:Team_Rocket
gptkbp:aircraft_operated gptkb:Soyuz-2
gptkbp:application launch vehicles
gptkbp:check_in_time 150 seconds
gptkbp:collaboration used in international missions
gptkbp:combustor_type staged combustion
gptkbp:cooling_system regenerative cooling
gptkbp:debut multiple launches since 1967
gptkbp:design_features modular design
gptkbp:design_influence influenced other rocket engines
gptkbp:designed_by gptkb:Kuznetsov_Design_Bureau
gptkbp:development gptkb:Soviet_Union
5 years
gptkbp:engine electric starter
staged combustion cycle
controlled shutdown
gptkbp:engine_configuration twin-engine
gptkbp:engine_type gptkb:Team_Rocket
gptkbp:environmental_impact low emissions
gptkbp:exhaust_system converging-diverging nozzle
gptkbp:first_flight gptkb:1967
gptkbp:fuel_economy high efficiency
gptkbp:fuel_type kerosene
gptkbp:future_prospects potential upgrades
gptkbp:has_documentation available for engineers
https://www.w3.org/2000/01/rdf-schema#label RD-0110 engines
gptkbp:ignition_system hypergolic
gptkbp:investment 10 MPa
gptkbp:is_tested_for static fire tests
gptkbp:launch_price cost-effective
gptkbp:legacy proven technology
gptkbp:manufacturer gptkb:Kuznetsov_Design_Bureau
gptkbp:number_of_rooms two
single combustion chamber
gptkbp:operational_use crew and cargo missions
gptkbp:oxidation_states liquid oxygen
gptkbp:performance high reliability
gptkbp:propulsion 100 k N
333:1
gptkbp:replaced_by gptkb:RD-0124
gptkbp:research_and_development ongoing improvements
gptkbp:safety_record excellent safety record
gptkbp:specific_impulse 300 seconds
gptkbp:status in service
gptkbp:type liquid-fueled
gptkbp:used_in gptkb:Soyuz_spacecraft
gptkbp:water_requirement 0.5 kg/s
1.0 kg/s
gptkbp:weight 300 kg
gptkbp:bfsParent gptkb:Progress_M-67_M
gptkbp:bfsLayer 7