Lada Land VM-01
Jump to navigation
Jump to search
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
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
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
External links
- "Легкий многоцелевой вертолет ВМ-01". авиару.рф.
- "Вертолет Лада Лэнд ВМ-01". Russianplanes.net.
Categories:
- CS1 Russian-language sources (ru)
- Use dmy dates from December 2022
- Articles with short description
- Short description is different from Wikidata
- Use American English from December 2022
- All Wikipedia articles written in American English
- Articles containing Russian-language text
- 2000s Russian civil utility aircraft
- 2000s Russian helicopters
- Aircraft manufactured in Russia
- All stub articles
- 2000s aircraft stubs