VRT 500
| Company type | Subsidiary |
|---|---|
| Industry | Aerospace |
| Parent | Russian Helicopters |
The VRT 500 represents a light helicopter design featuring a coaxial rotor configuration, developed by VR Technologies (VRT), which operates under the umbrella of Russian Helicopters.
Development
The project was initially revealed in March 2007, with a full-scale mock-up showcased during the 2017 MAKS airshow. Russian type certification was anticipated around 2017, while serial manufacturing was expected to commence between 2020 and 2021. In 2018, the rotor system underwent structural testing prior to aerodynamic evaluations, and the production of a prototype was planned by the end of that year. The VRT 500 aims to capture approximately 15% of the global civil market segment under two tons, targeting sales of around 700 units by 2030. The maiden flight was projected for 2019, with potential sales reaching up to 1,000 helicopters by 2035.
In August 2019, Malaysian firm Ludev Aviation placed an order for five units. During the November 2019 Dubai Air Show, Abu Dhabi’s investment group Tawazun declared intentions to acquire a 50% stake in VR-Technologies in early 2020. Concurrently, Swedish company Rotorcraft Nordic AB confirmed an order for ten helicopters. At this event, the selection of the Pratt & Whitney Canada PW207V engine was also announced.
Manufacturing will take place near Rome, Italy, with certification aimed at meeting European Union Aviation Safety Agency (EASA) standards similar to those applied to the Kamov Ka-32, particularly for firefighting and aerial utility roles. The development budget is estimated at €400 million (approximately $440 million), with the first flight targeted for 2020 and type certification expected by 2022. Starting in 2023, a hybrid propulsion option featuring a battery pack capable of powering the helicopter for three to five minutes may be introduced to comply with urban regulations restricting single-engine helicopters. Additionally, there is potential for establishing a production facility within the United Arab Emirates.
Design
This single-engine helicopter is equipped with dual three-blade coaxial rotor systems.[1] The preferred Western engine option is the Safran Arrius.[2] Its main blades are crafted from shaped carbon fiber to minimize noise output, complemented by a composite airframe, a glass cockpit, and sliding doors at the rear cabin. This model is designed to rival helicopters such as the Bell 505 and Robinson R66.[3] The VRT500 will be available in various variants, including passenger, utility, cargo, training, VIP, and Medevac configurations featuring rear cabin door loading.[4] It supports a maximum payload of 730 kg,[3] can achieve speeds up to 250 km/h, and has a flight range extending to 860 km.[5]
Weighing approximately 1.65 t (3,600 lb), this helicopter boasts a metallic airframe with composite skin panels and is powered by a single Pratt & Whitney PW207V engine, the same as that used in the Ansat light twin. The distinctive coaxial rotor, a hallmark of the Kamov Design Bureau, enables a compact fuselage design, simplifies ground handling, and reduces noise levels—features beneficial for urban transport. Italian automotive design firm Italdesign contributes to the aesthetic and ergonomic aspects, while avionics are supplied by Thales and environmental control systems come from Liebherr. Positioned in the $1–2 million price bracket, it competes with helicopters like the Bell 505 Jet Ranger X, Robinson R66, and Enstrom 480, offering a more spacious cabin.[6]
Configurations
Beyond its standard layout, the VRT500 offers several specialized configurations:[7][8]
- Passenger or air taxi: accommodates up to five energy-absorbing seats for passengers, with a luggage compartment accessible either from inside the cabin or via rear doors
- Cargo: supports payloads up to 730 kg within a volume of 5.3 m3, includes a courier seat, and offers a monitored sling load capacity of up to 900 kg
- Corporate: features two premium seats accompanied by a rear console or customizable VIP interiors upon request
- Public safety: equipped with external speakers, searchlight, thermal imaging camera, and other mission-specific devices integrated through avionics running non-certified software; interior simplified with up to five shoulder harnesses
- Medical evacuation: outfitted with a medical module featuring specialized flooring and lining, medical cabinet, equipment mounts, standardized stretchers loaded through rear doors, oxygen cylinder holders, medical spotlights, paramedic seating, and facilities for in-flight medical care
- Training: includes a simplified cabin interior with an optional removable second control set for instructor use
Specifications
Source: Aviation International News
- Passenger capacity: six individuals
- Payload capability: 730 kg (1,610 lb)
- Maximum takeoff weight: 1,600 kg (3,527 lb)
- Cruise speed: 230 km/h (124 kn)
- Top speed: 250 km/h (130 kn)
- Service ceiling altitude: 6,100 m (20,000 ft)
- Operational range: 860 km (460 nautical miles)
- Overall width: 8.09 m (26.5 ft) measured across engine pods
- Height dimension: 3.77 m (12.4 ft)
See also
Comparable designs
- Kamov Ka-26, featuring coaxial rotors with three blades and twin piston engines, equipped with a modular mission cabin
- Kamov Ka-126, a single-engine variant derived from the Ka-26
- Kamov Ka-226, an evolution with twin engines
Market competitors
References
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