Klimov M-100

E943288

The Klimov M-100 was a Soviet liquid-cooled V-12 aircraft engine developed in the 1930s as a domestically produced powerplant for fighters and bombers.

All labels observed (2)

Label Occurrences
Klimov M-103 2
Klimov M-100 canonical 1

How this entity was disambiguated

Statements (38)

Predicate Object
instanceOf V-12 engine
aircraft engine
piston engine
application military aviation
basedOn Hispano-Suiza 12Y
coolant water-glycol mixture
coolingSystem liquid-cooled
countryOfOrigin Soviet Union
cylinderArrangement V
cylinderCount 12
designGoal domestically produced powerplant
powerplant for bombers
powerplant for fighters
developer Vladimir Klimov NERFINISHED
engineConfiguration V-12
era 1930s
fuelType aviation gasoline
ignitionSystem dual ignition
manufacturer Klimov Design Bureau
notableFeature helped establish Soviet liquid-cooled engine industry
license-derived from foreign design
numberOfStrokes four-stroke
powerOutput approximately 750 hp
productionStatus out of production
propulsionType propeller-driving piston engine
serviceEntry mid-1930s
successor Klimov M-103
linked to: Klimov M-100

Klimov M-105
usedBy Soviet Air Force
linked to: Soviet Air Forces
usedDuring early World War II
pre–World War II period
usedFor bomber aircraft
fighter aircraft
usedIn Polikarpov I-16
Tupolev SB
early Soviet bombers
early Soviet fighters
valvetrain overhead camshaft

How these facts were elicited

Referenced by (3)

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

Hispano-Suiza 12Y licenseBuiltVariant Klimov M-100
subject linked to: Hispano-Suiza 12Y engine
Hispano-Suiza 12Y licenseBuiltVariant Klimov M-103
subject linked to: Hispano-Suiza 12Y engine
linked to: Klimov M-100
Klimov M-100 successor Klimov M-103
linked to: Klimov M-100