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In 1989 EliSport, which became Heli-Sport in 1997, bought the rights to the Cicare CH-6, a small single-seat open cockpit helicopter designed in Argentina by Augusto Cicaré. It was developed by Josi and Claudio Barbero and, with the help of the sports car designer, Marcello Gandini who produced a new, enclosed cabin, marketed from 1992 as the ...
The two-bladed rotor is of bonded metal construction. [1] The tail unit is attached by a pair of aluminum centreline booms. The upper one is mounted directly on the vertical engine/rotor mast and is cranked near midpoint to clear the propeller tips. The lower one is attached well below the keel on an extension plate.
The Wasp is a traditional pod and boom helicopter with a twin-blade rotor powered by a 90shp (97 kW) Garrett JFS-100-13A turboshaft engine. [1] It has a fixed skid landing gear and enclosed cabin with two-seat side-by-side seats. [1]
It also reportedly makes greater use of titanium and composites in its rotor blades and rotor, [4] and replaces the Z-8's boat-shaped lower fuselage with a tail ramp for small vehicles. [1] It has a glass cockpit [2] and is powered by three WZ-6C turboshafts. [2] [1] The Z-18's maximum takeoff weight (MTOW) is 13.8 tonnes.
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The aircraft has a standard empty weight of 234 lb (106 kg). It features a single main rotor and tail rotor, a single-seat, open cockpit without a windshield, skid landing gear with ground handling wheels. [1] The rotor is driven by tip jets fueled by hydrogen peroxide, which emits only water vapour and oxygen as exhaust products. The tail ...
The aircraft was designed long before the adoption of the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg), but nonetheless complies with them. The aircraft has a standard empty weight of 150 lb (68 kg) and is billed as the "World's Tiniest Homebuilt Helicopter" by the plans supplier.
Its low weight and compact size allows an ultralight certification. [3] To recover without autorotation, the Zefhir is fitted with a ballistic parachute safety system. [3] It is stored in a non-rotating box above the main rotor, attached to the airframe through a fixed shaft inside the rotor mast. [6] Other systems includes a glass cockpit. [1] [3]