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YAKOVLEV
YAKOVLEV YAK-100 |
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Este fue el segundo helicóptero de Yakovlev, utilizando en este caso un esquema convencional de rotor principal y rotor de cola. Solo se construyeron dos prototipos, pasando las pruebas en 1950, pero para esa época el MI-1 ya estaba en producción, y el YAK-100 fue abandonado. |
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The second Yakovlev's helicopter, using a conventional scheme with one main rotor and tail rotor for control and stability. Two prototypes built, test passed completely in 1950. But at the time extremely siccessful MI-1 was already in production, and Yak-100 project was closed. "History of aircraft construction in the USSR" by
V.B.Shavrov |
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Characteristics |
Information |
Characteristics |
Information |
First Flight Primer Vuelo |
1950 | Engine Motor |
1 AI-26GRFL |
Seating Capacity Plazas |
1 / 1 |
Power Potencia |
420 / 575 HP |
Empty Weight Peso Vacío |
3725 Lb |
Hover Ceiling
O.G.E. Estacionario O.G.E |
NA |
Maximum
Weight Peso Máximo |
4607 Lb |
Hover Ceiling
I.G.E. Estacionario I.G.E |
8242 Ft |
Vel. Cruise Vel. crucero |
NA |
Service
Ceiling Techo de Servicio |
17000 Ft |
V.N.E. V.N.E |
90 Kts |
Maximum
Range (Std) Alcance (Std) |
175 NM |
Dimensions / Dimensiones |
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Fuselage
Length Fuselaje Largo |
NA |
Main
Rotor Diameter Diam. Rotor Principal |
47,57 ft |
Length,
Rotors Turning Dist. Rotores Girando |
NA |
Tail
Rotor Diameter Diam. Rotor de Cola |
NA |
Total
Height Alto Total |
NA |
Price Precio |
NA |
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