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Antonov TR-301 |
zł 1.436.534
US$ 400.000 |
Przegląd
| Informacje podstawowe | | Typ: | Samolot jednośmigłowy | | Producent: | Antonov | | Model: | TR-301 | | Rok produkcji: | 2026 | | Lokalizacja: | Rosja, Yeisk | | Całkowity czas (TTAF): | 10 h | | Cena: | US$ 400.000
(~ zł 1.436.534) | | Wszystkie szczególy |
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Szczególy
| Informacje podstawowe | | Typ: | Samolot jednośmigłowy | | Producent: | Antonov | | Model: | TR-301 | | Rok produkcji: | 2026 | | Lokalizacja: | Rosja, Yeisk | | Całkowity czas (TTAF): | 10 h | | Cena: | US$ 400.000
(~ zł 1.436.534) |
| Silnik(i) | | Liczba silników: | 1 | | Producent/Model: | ASH62TR | | Zasilanie/Moc: | 1160 PS | | Czas całkowity: | 10 h |
| Opis/Charakterystyka silnika | The TR-301 aircraft, which was developed on the basis of the An-2 universal aircraft, but with many significantly better characteristics. Can be used from unpaved areas. At approximately the same speeds, payload of 1800 kg, cabin dimensions as the An-2, the TR-301 aircraft: 500 kg lighter than the An-2,
Engine ASh-62TR 1160hp with injection injection, overhaul life is 1000 hours.
consumes AI-95 gasoline,
gasoline consumption is 40% lower than An-2,
oil consumption is reduced by 3 times
one pilot
maintenance as it is, no calendars or resources.
Aircraft specifications:
Maximum takeoff weight - 4600 kg
The empty weight of the aircraft is 2900kg.
Crew: 1 person
Passenger capacity: up to 12 people.
Maximum speed: 270 km / h
Cruising speed: 190-220 km / h
Service ceiling: 4200 m
Climb rate: up to 6.5 m / s
Take-off run: 400 m
Fuel quantity - 1200 l
Gasoline consumption at cruising speed 120 l / h
Practical range: more than 1800 km.
It is possible to design and manufacture floats ... To a height of 4 km with 12 parachutists it will take 18-20 minutes! |
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