|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
space launch vehicles
potential for new missions
|
|
gptkbp:collaborations
|
international partnerships
|
|
gptkbp:combustor_type
|
staged combustion
3,000 K
|
|
gptkbp:control_system
|
gptkb:electronic
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:cultural_impact
|
featured in documentaries
|
|
gptkbp:debut
|
gptkb:1965
|
|
gptkbp:designed_by
|
gptkb:Kuznetsov_Design_Bureau
|
|
gptkbp:development
|
gptkb:Soviet_Union
1955-1965
|
|
gptkbp:diameter
|
1.5 m
|
|
gptkbp:educational_use
|
case studies in engineering
|
|
gptkbp:engine
|
electric
controlled
closed cycle
|
|
gptkbp:engine_configuration
|
single chamber
|
|
gptkbp:environmental_impact
|
low
|
|
gptkbp:facilities
|
gptkb:Gromov_Flight_Research_Institute
|
|
gptkbp:first_flight
|
gptkb:1966
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
kerosene
turbopump
|
|
gptkbp:has_documentation
|
extensive technical manuals
|
|
gptkbp:historical_significance
|
important in space exploration
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-0255 engine
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:invention
|
multiple patents filed
|
|
gptkbp:investment
|
15 bar
|
|
gptkbp:involved_technology
|
gptkb:advanced_propulsion_systems
|
|
gptkbp:launch_price
|
moderate
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launched
|
over 100
|
|
gptkbp:legacy
|
influenced future designs
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:manufacturer
|
gptkb:Kuznetsov
|
|
gptkbp:number_of_rooms
|
gptkb:1
|
|
gptkbp:operational_use
|
manned space missions
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:oxidizer_pump_type
|
turbopump
|
|
gptkbp:propulsion
|
yes
20:1
25,000 lbf
|
|
gptkbp:publications
|
numerous research papers
|
|
gptkbp:related_to
|
gptkb:RD-0125_engine
|
|
gptkbp:reliability
|
high
|
|
gptkbp:research_and_development
|
ongoing improvements
|
|
gptkbp:specific_impulse
|
300 seconds
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:RD-0120
|
|
gptkbp:type
|
liquid-fueled
|
|
gptkbp:used_in
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:valve_configuration
|
solenoid
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Viktor_Mikhailovich_Glushko
|
|
gptkbp:bfsLayer
|
6
|