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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:application
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gptkb:military_aircraft
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gptkbp:compression_ratio
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6.5:1
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gptkbp:configuration
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V-type
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gptkbp:control_system
|
mechanical control
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gptkbp:cooling_system
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liquid-cooled
water-cooled
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gptkbp:country_of_origin
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gptkb:Romania
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gptkbp:displacement
|
12.5 liters
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gptkbp:engine
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electric starter
developed in the late 1940s.
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gptkbp:engine_configuration
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gptkb:V6
cradle mount
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gptkbp:engine_intake
|
naturally aspirated
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gptkbp:engine_power
|
600 horsepower
reliable engine
high performance for its class
1500 hours
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gptkbp:engine_type
|
reciprocating engine
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gptkbp:exhaust_system
|
single exhaust
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gptkbp:first_flight
|
1950
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gptkbp:fuel_capacity
|
0.9 m
1.8 m
0.5 m
300 kilograms
|
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gptkbp:fuel_economy
|
40 liters/hour
|
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gptkbp:fuel_type
|
aviation gasoline
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|
https://www.w3.org/2000/01/rdf-schema#label
|
IAR 823 engine
|
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gptkbp:ignition_system
|
magneto ignition
|
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gptkbp:maintenance
|
periodic maintenance required
|
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gptkbp:manufacturer
|
IAR
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gptkbp:number_of_engines
|
gptkb:6
|
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gptkbp:power_output
|
600 hp
|
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gptkbp:production_years
|
1950-1955
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gptkbp:propeller
|
variable-pitch propeller
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gptkbp:successor
|
gptkb:IAR_860_engine
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gptkbp:torque
|
wet sump
1200 Nm
1200 Newton-meters
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|
gptkbp:type
|
piston engine
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gptkbp:used_in
|
IAR 823 aircraft
|
|
gptkbp:valve_configuration
|
overhead valves
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gptkbp:weight
|
300 kg
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gptkbp:bfsParent
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gptkb:IAR_823
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gptkbp:bfsLayer
|
8
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