RD-33-2

GPTKB entity

Predicate	Object
gptkbp:instance_of	gptkb:Team_Rocket
gptkbp:aircraft_operated	gptkb:Mikoyan_Mi_G-35
gptkbp:application	gptkb:fighter_aircraft
gptkbp:average_temperature	up to 1500 ° C
gptkbp:combustor_type	dual-spool turbojet
gptkbp:control_system	digital control system
gptkbp:cooling_system	air-cooled
gptkbp:country_of_origin	gptkb:Russia
gptkbp:designed_by	gptkb:Moscow_Institute_of_Thermal_Technology
gptkbp:development	gptkb:Soviet_Union 1970s
gptkbp:diameter	1.1 m
gptkbp:emissions_standard	low
gptkbp:engine	gptkb:RD-33_family gptkb:RD-33-1 mixed flow
gptkbp:engine_configuration	twin-engine afterburner thrust 98 k N
gptkbp:engine_power	2000 hours
gptkbp:engine_type	turbofan afterburning turbofan
gptkbp:exhaust_system	variable area nozzle
gptkbp:first_flight	gptkb:1977
gptkbp:fuel_capacity	3.2 m 1.1 m 300 kg
gptkbp:fuel_economy	0.8 kg/k N/h
gptkbp:fuel_type	kerosene
https://www.w3.org/2000/01/rdf-schema#label	RD-33-2
gptkbp:ignition_system	gptkb:spark_plug
gptkbp:length	3.2 m
gptkbp:maintenance	moderate
gptkbp:max_speed	Mach 2.25
gptkbp:noise_level	moderate
gptkbp:number_of_rooms	annular
gptkbp:operational_range	high
gptkbp:operational_use	gptkb:military_aircraft
gptkbp:oxidation_states	liquid oxygen
gptkbp:propulsion	no 0.27 81 k N
gptkbp:reliability	high
gptkbp:service_ceiling	15,000 m
gptkbp:specific_impulse	290 s
gptkbp:status	in production
gptkbp:successor	gptkb:RD-33_MK
gptkbp:used_in	gptkb:Mikoyan_Mi_G-29
gptkbp:variant	gptkb:RD-33-3
gptkbp:weight	300 kg
gptkbp:bfsParent	gptkb:RD-33_series
gptkbp:bfsLayer	8