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
|