Mil Mi-34
E649846
The Mil Mi-34 is a light, piston-engined Russian helicopter used primarily for training, sport flying, and utility roles.
Statements (48)
| Predicate | Object |
|---|---|
| instanceOf |
helicopter
ⓘ
light helicopter ⓘ piston-engined helicopter ⓘ |
| category | rotorcraft ⓘ |
| countryOfOrigin |
Russia
ⓘ
Soviet Union ⓘ |
| crew | 1 ⓘ |
| cruiseSpeed | 180 km/h ⓘ |
| designBureau | Mil Design Bureau NERFINISHED ⓘ |
| designedFor |
aerobatic training
ⓘ
civil aviation ⓘ military training ⓘ |
| developedIn | 1980s ⓘ |
| emptyWeight | 900 kg ⓘ |
| engineModel | Vedeneyev M-14V26 NERFINISHED ⓘ |
| engineType | piston engine ⓘ |
| firstFlight | 1986 ⓘ |
| fuselageMaterial |
composite materials
ⓘ
steel tube ⓘ |
| hasVariant |
Mil Mi-34A
NERFINISHED
ⓘ
Mil Mi-34C1 NERFINISHED ⓘ Mil Mi-34P NERFINISHED ⓘ Mil Mi-34S NERFINISHED ⓘ Mil Mi-34V NERFINISHED ⓘ |
| height | 3.1 m ⓘ |
| introduced | 1993 ⓘ |
| landingGearType | skid landing gear ⓘ |
| length | 11.0 m ⓘ |
| mainRotorDiameter | 10.0 m ⓘ |
| manufacturer | Mil Moscow Helicopter Plant NERFINISHED ⓘ |
| maxSpeed | 215 km/h ⓘ |
| maxTakeoffWeight | 1350 kg ⓘ |
| numberOfEngines | 1 ⓘ |
| passengerCapacity | 3 ⓘ |
| powerplantPower | 325 hp ⓘ |
| primaryUse |
sport flying
ⓘ
training helicopter ⓘ utility helicopter ⓘ |
| range | 430 km ⓘ |
| rateOfClimb | 8 m/s ⓘ |
| role |
aerobatic display
ⓘ
light utility transport ⓘ pilot training ⓘ |
| rotorConfiguration | single main rotor ⓘ |
| serviceCeiling | 3000 m ⓘ |
| tailRotor | conventional tail rotor ⓘ |
| usedBy |
Russian civil operators
ⓘ
Russian military training units ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.