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