Nakajima Sakae 11

E97798

The Nakajima Sakae 11 was an early variant of Nakajima's air-cooled radial aircraft engine used in several Japanese military aircraft during the Second World War.

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Observed surface forms (1)

Surface form Occurrences
Nakajima Sakae 21 1

Statements (44)

Predicate Object
instanceOf aircraft engine
piston engine
radial engine
application fighter aircraft
torpedo bomber
bore 130 mm
coolingSystem air‑cooled
coolingType forced‑air baffle cooling
countryOfOrigin Japan
cylinderArrangement double‑row radial
designGoal lightweight high‑power engine for carrier fighters
displacement 1704 in³
27.9 L
engineConfiguration air‑cooled radial
era 1930s
1940s
family Nakajima Sakae NERFINISHED
fuelType aviation gasoline
ignitionSystem dual ignition
manufacturer Nakajima Aircraft Company
nationality Japanese
notableUse early production Mitsubishi A6M Zero fighters
numberOfCylinders 14
powerOutput 701 kW
940 hp
powerOutputRpm 2400 rpm
predecessor Nakajima Hikari
productionPeriod early 1940s
late 1930s
role aircraft powerplant
stroke 150 mm
successor Nakajima Sakae 12
Nakajima Sakae 11 self-linksurface differs
surface form: Nakajima Sakae 21
supercharging single‑stage supercharger
takeoffPower 940 hp at takeoff
usedBy Imperial Japanese Army Air Service
Imperial Japanese Navy
usedInAircraft Mitsubishi A6M2 Zero NERFINISHED
Nakajima B5N2 Kate NERFINISHED
Nakajima Ki‑43 prototype
usedInConflict World War II
surface form: Second World War
usedInTheater Pacific War
valvetrain overhead valve
variantOf Nakajima Sakae radial engine
surface form: Nakajima Sakae engine family

Referenced by (2)

Full triples — surface form annotated when it differs from this entity's canonical label.

Nakajima B5N torpedo bombers powerplant Nakajima Sakae 11
subject surface form: Nakajima B5N
Nakajima Sakae 11 successor Nakajima Sakae 11 self-linksurface differs
this entity surface form: Nakajima Sakae 21