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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:aircraft_operated
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gptkb:de_Havilland_DH.89_Dragon_Rapide
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gptkbp:application
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gptkb:trainer_aircraft
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gptkbp:compression_ratio
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6.5:1
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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:United_Kingdom
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gptkbp:displacement
|
6.5 liters
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gptkbp:engine
|
gptkb:Gipsy_series
used in various aircraft models
dual ignition
developed in the 1930s
influenced future aircraft engine designs
produced in limited numbers.
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gptkbp:engine_configuration
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gptkb:V8_engine
V-type engine
horizontally opposed
detailed specifications available
Gipsy 6
designed for light aircraft use
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|
gptkbp:engine_power
|
150-200 hp
high reliability
good performance at altitude
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gptkbp:engine_type
|
reciprocating engine
Gipsy Six A
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gptkbp:first_flight
|
1930s
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gptkbp:fuel_capacity
|
1 meter
1.5 meters
0.9 meters
150-200 kg
0.8 meters
|
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gptkbp:fuel_type
|
gptkb:carburetor
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Gipsy Six Series II
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gptkbp:ignition_system
|
magneto ignition
|
|
gptkbp:maintenance
|
regular inspections required
|
|
gptkbp:manufacturer
|
gptkb:de_Havilland
|
|
gptkbp:max_speed
|
2500 rpm
|
|
gptkbp:number_of_engines
|
six-cylinder
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|
gptkbp:power_output
|
200 hp
|
|
gptkbp:production_years
|
1930s to 1940s
|
|
gptkbp:propeller
|
variable-pitch propeller
|
|
gptkbp:replaced_by
|
gptkb:Gipsy_Major
|
|
gptkbp:successor
|
gptkb:Gipsy_Queen
|
|
gptkbp:torque
|
400 Nm
300-400 Nm
|
|
gptkbp:type
|
inline engine
|
|
gptkbp:used_in
|
gptkb:light_aircraft
|
|
gptkbp:valve_configuration
|
overhead valves
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|
gptkbp:weight
|
approximately 150 kg
|
|
gptkbp:bfsParent
|
gptkb:Gipsy_Six_engine
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gptkbp:bfsLayer
|
9
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