Lada Land VM-01
| VM-01 | |
|---|---|
| Role | Light utility helicopter |
| Manufacturer | Lada Land |
| First flight | May 2001 |
| Number built | 1 |
The VM-01 (Russian: ВМ-01) is a light helicopter from the Lada Land (Russian: Лада Лэнд) company in Tolyatti, Russia. The design was created privately by the company, but production was assisted by OKB Mil and Kamov.[1]
Design
[edit]The aircraft contains a rotary-piston engine, four-bladed main rotor, two-bladed tail rotor, skid undercarriage, titanium alloys in the construction of the load system, and composite materials in the fuselage construction. The first flight was in May, 2001.
Specifications
[edit]General characteristics
- Crew: 1
- Capacity: 2 (1 pilot + 1 passenger)
- Max takeoff weight: 830 kg (1,830 lb)
- Powerplant: 1 × PD VAZ-413 rotary piston engine, 112 kW (150 hp)
- Main rotor diameter: 9 m (29 ft 6 in)
Performance
- Cruise speed: 140 km/h (87 mph, 76 kn)
- Range: 330 km (210 mi, 180 nmi)
- Service ceiling: 3,000 m (9,800 ft)
- Rate of climb: 4 m/s (790 ft/min)
References
[edit]External links
[edit]- "Легкий многоцелевой вертолет ВМ-01". авиару.рф.
- "Вертолет Лада Лэнд ВМ-01". Russianplanes.net.
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Credit:
(see original file).
