Engineering:Apollo Jet Star
| Jet Star | |
|---|---|
| Role | Ultralight trike |
| National origin | Hungary |
| Manufacturer | Apollo Ultralight Aircraft |
| Status | In production (2013) |
The Apollo Jet Star is a Hungarian ultralight trike, designed and produced by Apollo Ultralight Aircraft of Eger. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.[1]
Design and development
The Jet Star was designed to comply with the Fédération Aéronautique Internationale microlight category as well as the US light-sport aircraft category. It features a cable-braced or strut-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem, open cockpit, tricycle landing gear with wheel pants and a single engine in pusher configuration.[1]
The Jet Star is accepted in the United States as both an Experimental and Special Light-sport aircraft.[2]
The aircraft is made from bolted-together aluminum tubing, with its double surface wing covered in Dacron sailcloth. The aircraft uses an "A" frame weight-shift control bar. The main landing gear uses strut-type suspension, rather than the leaf-type suspension used on the Apollo Delta Jet series. The powerplant options include the twin cylinder, liquid-cooled, two-stroke, dual-ignition 64 hp (48 kW) Rotax 582 engine, the four cylinder, air and liquid-cooled, four-stroke, dual-ignition 80 hp (60 kW) Rotax 912 or 100 hp (75 kW) Rotax 912S engine.[1]
The aircraft has an empty weight of 180 kg (397 lb) and a gross weight of 430 kg (948 lb), giving a useful load of 250 kg (551 lb). With full fuel of 45 litres (9.9 imp gal; 12 US gal) the payload is 218 kg (481 lb).[1]
A number of different wings can be fitted to the basic carriage, including the cable-braced Aeros Profi, the cable-braced Air Creation iXess, the strut-braced Aeros Profi TL or the strut-braced Gibbogear Manta Ray 12.5.[1]
Specifications (Jet Star)
Data from Bayerl[1]
General characteristics
- Crew: one
- Capacity: one passenger
- Wingspan: 9.5 m (31 ft 2 in)
- Wing area: 15 m2 (160 sq ft)
- Empty weight: 180 kg (397 lb)
- Gross weight: 430 kg (948 lb)
- Fuel capacity: 45 litres (9.9 imp gal; 12 US gal)
- Powerplant: 1 × Rotax 912UL four cylinder, liquid and air-cooled, four stroke aircraft engine, 60 kW (80 hp)
- Propellers: 3-bladed composite
Performance
- Maximum speed: 125 km/h (78 mph, 67 kn)
- Cruise speed: 110 km/h (68 mph, 59 kn)
- Stall speed: 55 km/h (34 mph, 30 kn)
- Rate of climb: 4 m/s (790 ft/min)
- Wing loading: 28.7 kg/m2 (5.9 lb/sq ft)
References
- ↑ 1.0 1.1 1.2 1.3 1.4 1.5 Bayerl, Robby; Martin Berkemeier; et al.: World Directory of Leisure Aviation 2011-12, page 205. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ↑ Federal Aviation Administration (7 January 2013). "SLSA Make/Model Directory". Archived from the original on 16 May 2013. https://web.archive.org/web/20130516004527/http://www.faa.gov/aircraft/gen_av/light_sport/media/SLSA_Directory.xls. Retrieved 17 April 2013.
External links
 |  |
