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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]
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.
The Hiller ROE Rotorcycle is a single-seat ultralight helicopter designed in 1953 for a military requirement. [1] A total of 12 were produced for the United States Marine Corps. And in 1954, the Hiller Helicopters was selected by the US Navy's Bureau of Aeronautics to build this design of a one-man, foldable, self-rescue and observation ...
The A/W 95 features a single main rotor, a single-seat open cockpit without a windshield, skid-type landing gear and can accept engines of 50 to 75 hp (37 to 56 kW). The standard engine used is the twin cylinder, air-cooled, two-stroke, dual-ignition 50 hp (37 kW) Rotax 503 engine. The aircraft fuselage is made from bolted-together aluminum ...
The piston engine-powered CH-8 ultralight series use the traditional "penny-farthing" layout with two-bladed main and tail rotors. The main rotor is formed from composites and is a teetering, semi-rigid design with 6° of twist. The pod-and-boom fuselage has a carbon fiber and epoxy resin cabin with a long transparent forward-opening canopy.
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 ...
It features a single main rotor and tail rotor, a single-seat open cockpit without a windshield, tricycle landing gear with main wheels and nose skid and a twin cylinder, air-cooled, two-stroke, single-ignition 40 hp (30 kW) Rotax 447 aircraft engine or Kawasaki 440 snowmobile engine. The 50 hp (37 kW) Rotax 503 can also be used.
Data from Jane's All the World's Aircraft 2010/11 General characteristics Crew: two Length: 12 ft 3 in (3.73 m) fuselage Width: 6 ft 1 in (1.85 m) fuselage maximum Height: 10 ft 0 in (3.05 m) overall Empty weight: 899 lb (408 kg) Gross weight: 1,499 lb (680 kg) Fuel capacity: 87 L (19.2 Imp gal, 23.0 US gal) usable Powerplant: 1 × Subaru EJ25 flat four piston, 160 hp (119 kW) Main rotor ...
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