|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
satellite launches
|
|
gptkbp:average_temperature
|
1,000 K
|
|
gptkbp:collaborations
|
collaborations with universities
|
|
gptkbp:combustor_type
|
staged combustion
|
|
gptkbp:community_support
|
strong community support
|
|
gptkbp:competitors
|
competes with other rocket engines
|
|
gptkbp:conference
|
presented at aerospace conferences
|
|
gptkbp:control_system
|
digital control system
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:debut
|
multiple successful launches
|
|
gptkbp:design_features
|
modular design
|
|
gptkbp:designed_by
|
gptkb:Aerojet_Rocketdyne
|
|
gptkbp:development
|
gptkb:2000
gptkb:2005
|
|
gptkbp:development_cost
|
$50 million
|
|
gptkbp:diameter
|
1.5 m
|
|
gptkbp:educational_use
|
used in educational programs
|
|
gptkbp:emissions_standard
|
low emissions
|
|
gptkbp:engine
|
gptkb:RD-190_engine
gptkb:RD-180_engine
staged combustion cycle
|
|
gptkbp:environmental_impact
|
minimal environmental impact
|
|
gptkbp:exhaust_system
|
bell nozzle
|
|
gptkbp:facilities
|
NASA test facilities
|
|
gptkbp:first_flight
|
gptkb:2005
|
|
gptkbp:fuel_economy
|
high fuel efficiency
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-600 engine
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:invention
|
multiple patents filed
|
|
gptkbp:length
|
4.5 m
|
|
gptkbp:maintenance
|
low maintenance
|
|
gptkbp:manufacturer
|
gptkb:Aerojet_Rocketdyne
|
|
gptkbp:market
|
commercial space market
|
|
gptkbp:number_of_rooms
|
gptkb:1
3.5 MPa
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:part_of
|
launch vehicle system
|
|
gptkbp:performance
|
high performance
|
|
gptkbp:project
|
upgraded versions planned
|
|
gptkbp:propulsion
|
50:1
600 k N
|
|
gptkbp:publications
|
numerous technical publications
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:research_and_development
|
ongoing R& D efforts
|
|
gptkbp:safety_record
|
excellent safety record
|
|
gptkbp:simulation_models
|
available simulation models
|
|
gptkbp:specific_impulse
|
300 seconds
|
|
gptkbp:status
|
in production
|
|
gptkbp:trends
|
trends towards reusable engines
|
|
gptkbp:used_in
|
launch vehicles
|
|
gptkbp:user_countries
|
used internationally
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Klimov_design_bureau
|
|
gptkbp:bfsLayer
|
7
|