|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
launch vehicles
|
|
gptkbp:average_temperature
|
up to 3,000 K
|
|
gptkbp:check_in_time
|
approximately 150 seconds
|
|
gptkbp:combustion_chamber_material
|
titanium
|
|
gptkbp:combustor_type
|
staged combustion
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:country_of_origin
|
gptkb:Russia
|
|
gptkbp:critical_component
|
main propulsion system
|
|
gptkbp:design
|
10 years
Aviadvigatel engineers
|
|
gptkbp:development
|
1990s
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:engine
|
gas-generator cycle
|
|
gptkbp:engine_configuration
|
vertical
|
|
gptkbp:engine_power
|
up to 25 missions
|
|
gptkbp:engine_type
|
liquid-fueled
|
|
gptkbp:environmental_impact
|
low emissions
|
|
gptkbp:exhaust_system
|
bell nozzle
|
|
gptkbp:exported_to
|
gptkb:United_States
|
|
gptkbp:first_flight
|
gptkb:2000
|
|
gptkbp:first_introduced
|
gptkb:Atlas_III
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_mixture_ratio
|
2.5:1
|
|
gptkbp:fuel_type
|
RP-1 and liquid oxygen
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Russia's RD-180 engine
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:influenced_by
|
gptkb:RD-170
|
|
gptkbp:inspired_by
|
Soviet rocket technology
|
|
gptkbp:invention
|
gptkb:Aviadvigatel
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral
|
|
gptkbp:launch_vehicle
|
gptkb:Atlas
|
|
gptkbp:manufacturer
|
gptkb:Aviadvigatel
|
|
gptkbp:notable_achievement
|
successful launches since 2000
|
|
gptkbp:notable_feature
|
high performance
dual combustion chamber design
|
|
gptkbp:notable_mission
|
gptkb:Mars_Science_Laboratory
|
|
gptkbp:number_of_engines
|
one or two
|
|
gptkbp:number_of_rooms
|
two
1,200 psi
|
|
gptkbp:operated_by
|
gptkb:NASA
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:operational_use
|
commercial and government missions
|
|
gptkbp:part_of
|
gptkb:Team_Rocket
|
|
gptkbp:propulsion
|
400,000 lbf
133:1
|
|
gptkbp:reliability
|
high
|
|
gptkbp:replaced_by
|
Vulcan Centaur engine
|
|
gptkbp:service
|
gptkb:2000
|
|
gptkbp:specific_impulse
|
311 seconds
|
|
gptkbp:successor
|
gptkb:RD-191
|
|
gptkbp:used_by
|
gptkb:United_Launch_Alliance
|
|
gptkbp:used_for
|
satellite launches
|
|
gptkbp:used_in
|
gptkb:Atlas
national security launches
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:bfsParent
|
gptkb:AR1_rocket_engine
|
|
gptkbp:bfsLayer
|
6
|