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The Celier Xenon 4 (also referred to by the manufacturer as the Xenon IV) is a Maltese autogyro designed by Raphael Celier and produced by Celier Aviation of Safi, Malta. The aircraft is supplied complete and ready-to-fly.[1]
| Xenon 4 | |
|---|---|
 | |
| Role | Autogyro |
| National origin | Malta |
| Manufacturer | Celier Aviation |
| Designer | Raphael Celier |
| Status | In production (2017) |
| Developed from | Celier Xenon 2 |
Design and development
The Xenon 4 is a development of the Celier Xenon 2 and Celier Xenon 3, with a newly designed fuselage and longer tailboom. It features a single main rotor, a two-seats-in side-by-side configuration enclosed cockpit, with some models offering a third seat. It has tricycle landing gear and a modified four cylinder, liquid and air-cooled, four stroke 135 hp (101 kW) turbocharged Rotax 912 engine in pusher configuration.[1][2]
The fuselage is a monocoque made from carbon fiber reinforced polymer and features a cabin internal width of 130 cm (51 in). The two-bladed rotor has a diameter of 8.8 m (28.9 ft) and a chord of 20 cm (7.9 in). The aircraft has a typical empty weight of 295 kg (650 lb) and a maximum gross weight of 560 kg (1,235 lb), giving a useful load of 265 kg (584 lb). With full fuel of 85 litres (19 imp gal; 22 US gal) the payload for the pilot, passengers and baggage is 205 kg (452 lb).[1]
Variants
- Xenon 4 Sport
- Entry level civil model with two seats in side-by-side configuration.[3]
- Xenon 4 XL
- Mid level civil model with three seats in 1-2 configuration.[2]
- Xenon 4 Executive
- Top level civil model with three seats in 1-2 configuration.[4]
- Xenon 4 Geo
- Civil model equipped for the land survey and aerial photography roles, intended for the construction, mining and survey industries.[5]
- C-22
- Military model for medevac and other military roles; also referred to as the C-44.[6]
- C-22 VIP
- Civil model for VIP transport.[7]
Specifications (Xenon 4 Executive)
Data from Tacke[1]
General characteristics
- Crew: one
- Capacity: two passengers
- Empty weight: 295 kg (650 lb)
- Gross weight: 560 kg (1,235 lb)
- Fuel capacity: 85 litres (19 imp gal; 22 US gal)
- Powerplant: 1 × Rotax 912ULS-T modified four cylinder, liquid and air-cooled, four stroke aircraft engine, 101 kW (135 hp)
- Main rotor diameter: 8.8 m (28 ft 10 in)
- Main rotor area: 61 m2 (660 sq ft)
- Propellers: 3-bladed composite
Performance
- Maximum speed: 195 km/h (121 mph, 105 kn)
- Cruise speed: 160 km/h (99 mph, 86 kn)
- Rate of climb: 5 m/s (980 ft/min)
- Disk loading: 9.1 kg/m2 (1.9 lb/sq ft)
See also
References
- Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 191. Flying Pages Europe SARL, 2015. ISSN 1368-485X
- Celier Aviation. "Xenon 4 XL". www.celiergroup.com. Archived from the original on 10 November 2017. Retrieved 10 November 2017.
- Celier Aviation. "Xenon 4 Sport". www.celiergroup.com. Archived from the original on 11 November 2017. Retrieved 10 November 2017.
- Celier Aviation. "Xenon 4 Executive". www.celiergroup.com. Archived from the original on 11 November 2017. Retrieved 10 November 2017.
- Celier Aviation. "Xenon 4 Geo". www.celiergroup.com. Archived from the original on 11 November 2017. Retrieved 10 November 2017.
- Celier Aviation. "C-22 Medevac". www.celiergroup.com. Archived from the original on 10 November 2017. Retrieved 10 November 2017.
- Celier Aviation. "C-22 VIP". www.celiergroup.com. Archived from the original on 11 November 2017. Retrieved 10 November 2017.
External links
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