The Kamov Ka-115 Moskvichka is a light multi-purpose helicopter designed for many uses, including passenger and cargo transportation, emergency service, SAR and patrol, or charter flights.
Development is based on extensive use of advanced technologies tested to ensure high performance and reduce operating costs. A full-scale mockup of the helicopter was first built to optimize the layout of technological, operational, and ergonomic features. A wind tunnel model TsAGI was created to test flight characteristics and improve aerodynamic airframe layout. Laboratories tested the air intakes' dust device to improve efficiency. A model of the Ka-115 was presented at the aerospace show MAKS-95 in Zhukovsky. Prototype's first flight was 1999 and the aircraft is in production.
The basic Ka-115 is powered by a Pratt & Whitney Canada/Klimov PW206K/2 engine that drives a coaxial rotor system, equipped with rotor de-icing. The Ka-115 features a large five-door cabin with large windows and a skid undercarriage. The cabin is fitted with vibration and noise suppression, heating and ventilation systems, and comfortable shock-absorbing crew and passenger seats.
Specificationsedit
General characteristics
Crew: 1
Capacity: 4 passengers or 900 kg (1,984 lb) maximum payload
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May 02, 2024
kamov, moskvichka, light, multi, purpose, helicopter, designed, many, uses, including, passenger, cargo, transportation, emergency, service, patrol, charter, flights, moskvichka, role, light, multi, purpose, helicopter, manufacturer, kamov, first, flight, 1999. The Kamov Ka 115 Moskvichka is a light multi purpose helicopter designed for many uses including passenger and cargo transportation emergency service SAR and patrol or charter flights Ka 115 Moskvichka Role light multi purpose helicopter Manufacturer Kamov First flight 1999 Status project Contents 1 Design and development 2 Specifications 3 References 4 External linksDesign and development editDevelopment is based on extensive use of advanced technologies tested to ensure high performance and reduce operating costs A full scale mockup of the helicopter was first built to optimize the layout of technological operational and ergonomic features A wind tunnel model TsAGI was created to test flight characteristics and improve aerodynamic airframe layout Laboratories tested the air intakes dust device to improve efficiency A model of the Ka 115 was presented at the aerospace show MAKS 95 in Zhukovsky Prototype s first flight was 1999 and the aircraft is in production The basic Ka 115 is powered by a Pratt amp Whitney Canada Klimov PW206K 2 engine that drives a coaxial rotor system equipped with rotor de icing The Ka 115 features a large five door cabin with large windows and a skid undercarriage The cabin is fitted with vibration and noise suppression heating and ventilation systems and comfortable shock absorbing crew and passenger seats Specifications editGeneral characteristics Crew 1 Capacity 4 passengers or 900 kg 1 984 lb maximum payload Length 9 2 m 30 ft 2 in Width 2 0 m 6 ft 7 in Height 3 6 m 11 ft 10 in Max takeoff weight 1 850 kg 4 079 lb Powerplant 1 Pratt amp Whitney Klimov PW 206K 2 turboshaft engine 477 kW 640 hp Main rotor diameter 9 5 m 31 ft 2 in Main rotor area 70 88 m2 762 9 sq ft Performance Maximum speed 250 km h 160 mph 130 kn Cruise speed 230 km h 140 mph 120 kn Range 780 km 480 mi 420 nmi Service ceiling 5 200 m 17 100 ft Rate of climb 11 5 m s 2 260 ft min References editwww airshow ru EI Ruzhitsky Helicopters 1997External links edit nbsp Wikimedia Commons has media related to Kamov Ka 115 www aviation ru www fsdome com www skycar co za Retrieved from https en wikipedia org w index php title Kamov Ka 115 amp oldid 1195624770, wikipedia, wiki, book, books, library,
