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gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Angara_rocket
|
|
gptkbp:application
|
launch vehicles
|
|
gptkbp:average_temperature
|
~3000 K
|
|
gptkbp:check_in_time
|
~200 s
|
|
gptkbp:collaborations
|
limited
|
|
gptkbp:controls
|
digital
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:debut_year
|
gptkb:2011
|
|
gptkbp:design
|
~10 years
|
|
gptkbp:designed_by
|
gptkb:Kuznetsov
|
|
gptkbp:developer
|
2000s
~100 million USD
|
|
gptkbp:diameter
|
2.4 m
|
|
gptkbp:durability
|
not reusable
|
|
gptkbp:emissions_standard
|
aerospike
|
|
gptkbp:engine
|
gptkb:RD-0124
gptkb:RD-180
gptkb:RD-0120
|
|
gptkbp:engine_type
|
staged combustion
liquid bipropellant
|
|
gptkbp:environmental_impact
|
low emissions
|
|
gptkbp:facilities
|
Kuznetsov test site
|
|
gptkbp:first_flight
|
gptkb:2014
|
|
gptkbp:fuel_type
|
staged combustion
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-191 engine
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:invention
|
multiple patents filed
|
|
gptkbp:key
|
modular design
advanced materials
high efficiency
high thrust-to-weight ratio
digital control system
|
|
gptkbp:launch_date
|
~2 per year
|
|
gptkbp:launch_site
|
gptkb:Russian_space_agency
|
|
gptkbp:length
|
4.5 m
|
|
gptkbp:manufacturer
|
gptkb:Kuznetsov
|
|
gptkbp:number_of_rooms
|
four
25 M Pa
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:propulsion
|
2.4
1900 k N
311 s
|
|
gptkbp:research_and_development
|
ongoing
|
|
gptkbp:safety_record
|
high safety record
|
|
gptkbp:social_structure
|
liquid oxygen
|
|
gptkbp:status
|
in service
|
|
gptkbp:upgrades
|
planned upgrades
|
|
gptkbp:used_in
|
gptkb:Angara_rocket
|
|
gptkbp:weight
|
800 kg
|