Search results
Results from the WOW.Com Content Network
The aircraft has a standard empty weight of 70 kg (154 lb). It features two contra-rotating main rotors, a single-seat open cockpit without a windshield, four-wheeled landing gear and four twin-cylinder, air-cooled, two-stroke , 10 hp (7 kW) GEN 125-F engines to provide operational redundancy since the aircraft cannot autorotate in the event of ...
The CoAX 2D/2R was originally known as the FLIP 2 (Fly In Perfection) and is a derivative of the FLIP 1, a conventional helicopter with a main and tail rotor.[1]The CoAX 2D/2R was designed to comply with the European Class 6 microlight helicopter rules, including the category's maximum takeoff weight of 450 kg (992 lb).
The aircraft has skid-type landing gear with removable wheels, [4] a glass fiber soundproof cabin with an aluminium tube frame inside taken from Ptenets-2 making a tail and boom structure. [ 3 ] The Cobra 500 parachute rescue system is located under the tail boom behinder the engine, if activated the helicopter will tilt forward which will the ...
Coaxial Single Seater [17] Shandong coax heli China Coaxial Single Seater [18] Guo Leiting's Coax China Yuncheng Farmer's Chopper Shantou Copters China Homebuilt Helis by Farmer Chen Ruihua Jiangsu China Coaxial Single Seater [19] Coaxial heli Zhuzhou China Coaxial Single Seater [20] Agricultural coaxial heli China [21] Red Coaxial Helicopter China
Single seat helicopters are helicopters have one place. A commonly known type of the helicopter that must be single seat, is the FAA Ultralight Helicopter, though single place helicopters existed before this classification (See Ultralight aircraft (United States))
The Livella Uno was designed to comply with the US FAR 103 Ultralight Vehicles and the European 120 kg class ultralight aircraft rules. It features a dual coaxial main rotors, with an inverted V-tail, a single open-air pilot's seat without a windshield, tricycle landing gear and a 40 hp (30 kW) Wankel Aixro XH40 engine. [1] The aircraft ...
The aircraft has a very small wing for the US ultralight category with a wing area of only 95 sq ft (8.8 m 2) and a wingspan of 17.6 ft (5.4 m). The wing is equipped with flaps that give it a stall speed of 25 mph (40 km/h). The small wing gives the aircraft a high cruise speed and better resistance to turbulence than a lighter-loaded wing.
Information from Jane's All the World's Aircraft 2010 [1] and manufacturer's website [2] CH-7 Angel CH-6 with new, enclosed cockpit, powered by either 48 kW (64 hp) Rotax 582UL UL or 60 kW (80 hp) Rotax 912 UL. First marketed in 1992, but kits no longer (2010) available. CH-7 Kompress