Armstrong Siddeley 100 HP

GPTKB entity

Properties (49)
Predicate Object
gptkbp:instanceOf aircraft engine
gptkbp:application military aircraft
gptkbp:compressionRatio 5.5:1
gptkbp:coolingSystem water-cooled
liquid cooling system
gptkbp:design inline configuration
gptkbp:displacement 1.8 liters
gptkbp:drivetrain overhead valves
gptkbp:engine training aircraft
horizontally opposed
influenced future designs
innovative design features
used in various military aircraft
designed for reliability and efficiency
gptkbp:engineConfiguration inline-four
produced in large numbers
100 hp at maximum performance
developed_during_WWI
gptkbp:enginePower 100 hp at 1,800 rpm
gptkbp:engineType lightweight design
reciprocating engine
multiple variants produced
different horsepower ratings
gptkbp:fuelType aviation gasoline
gptkbp:hasArea extensive testing conducted
https://www.w3.org/2000/01/rdf-schema#label Armstrong Siddeley 100 HP
gptkbp:introduced 1917
gptkbp:is_used_in various aircraft
gptkbp:manufacturer gptkb:Armstrong_Siddeley
gptkbp:notableFeature well-regarded in aviation circles
gptkbp:notableUsers gptkb:Royal_Air_Force
gptkbp:operationalHistory part of aviation history
gptkbp:performance reliable operation
gptkbp:performances high reliability
easy maintenance
detailed specifications available
long operational lifespan
good performance metrics
characteristics suited for training aircraft
specific performance metrics available
gptkbp:powers 100 horsepower
gptkbp:productionYears 1917-1925
gptkbp:related_engine four-stroke
Armstrong_Siddeley_Mongoose
gptkbp:setting 4-cylinder
gptkbp:successor gptkb:Armstrong_Siddeley_Lynx
gptkbp:torque varies with RPM
gptkbp:type inline engine
gptkbp:weight approximately 120 kg