Junkers Jumo 210

E746252

The Junkers Jumo 210 was an early German liquid-cooled, inverted V-12 aircraft engine widely used in pre–World War II and early-war Luftwaffe fighter prototypes and light aircraft.

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Label Occurrences
Junkers Jumo 210 canonical 1

Statements (46)

Predicate Object
instanceOf aircraft engine
liquid-cooled aircraft engine
piston engine
application dive bomber prototypes
single-engine fighters
bore 120 mm
configuration inverted V-12
coolingSystem liquid-cooled
countryOfOrigin Germany
cylinderArrangement V
cylinderCount 12
designGoal medium-power engine for modern monoplane fighters
developedFor Luftwaffe fighter program
displacement 19.7 L
approximately 1,200 cu in
era early World War II
interwar period
firstRun mid-1930s
fuelSystem carbureted
fuelType aviation gasoline
historicalSignificance one of the first modern German inverted V-12 aircraft engines of the 1930s
introduced 1934
manufacturer Junkers Motorenbau NERFINISHED
notableFeature four valves per cylinder for improved breathing
inverted V layout for improved pilot visibility
single-stage supercharger for altitude performance
powerOutput approximately 600 hp
between 610 and 730 PS depending on variant
primaryUse fighter prototypes
light aircraft
productionEnd late 1930s
productionStart 1934
replacedBy Daimler-Benz DB 601 in later Bf 109 variants NERFINISHED
stroke 140 mm
successor Junkers Jumo 211 NERFINISHED
supercharger single-stage supercharger
usedBy Luftwaffe
usedInAircraft Arado Ar 68 NERFINISHED
Heinkel He 112 NERFINISHED
Junkers Ju 87 prototypes NERFINISHED
Messerschmitt Bf 109 prototypes
early production Messerschmitt Bf 109 variants
various German trainer and light aircraft
usedInConflict World War II
usedInPeriod pre–World War II
valvetrain four valves per cylinder

Referenced by (1)

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

Heinkel He 112 powerplant Junkers Jumo 210