Antares 23 E | D-KULS The Antares 23E is the flagship of the Antares family. Being a completely new development, the Antares 23E combines innovative ideas and new, evolutionary and technologically advanced concepts to create the glider of the 21st century. The Antares 23E: - Optimal soaring performance, wide range in wingloading (39 kg/m2 - 58 kg/m2)
- Highly sensitive controls and good handling
- High performance with an almost silent propulsion system and comfortable and simple handling
- Exceptional reliability with maximum safety
- Low maintenance costs and very simple maintenance
- Last but not least: A very elegant aircraft
Technical data Geometry: | | | Weights: | | | | | | | | | | Wing span: | 23 m /75.5 ft | | | Empty weight: | ca. 535 kg / 1180 lb | | Wing area: | 14,75 m² / 159 ft² | | | MTOW: | 850 kg / 1874 lb | | Fuselage length: | 7.4 m / 24.3 ft | | | Water ballast: | 240 l / 63.4 US gallons | | Fuselage height: | 1,89 m / 6,4 ft | | | Min. Wingloading: | 38.6 kg/m² / 7.9 lb/ ft² | | Aspect ratio: | 38,5 | | | Max. Wingloading: | 57,6 kg/m² / 11.8 lb/ ft² | | Best Glide ratio: | 60 at 125 km/h mit 41,0 kg/m² at 145 km/h mit 57,6 kg/m² | | Powered performance: | | | Min. Sink rate at 600 kg / 1323 lb | 0,45 m/s / 89 ft/min | | | | | | Stall speed at 600 kg / 1323 lb | 73km/h / 39.4 kts | | | Max. climb rate at 600 kg / 1323 lb | 4 m/s / 790 ft/min | | | | | | Max. climb altitude at 600 kg / 1323 lb | 2850 m / 9350 ft | Propulsion data: | | | | Max. climb altitude at 850 kg / 1874 lb | 2000 m / 6560 ft | | | | | | | | | Motor: | DC/DC brushless | | | Built in | 2013 | | Power: | 42 kW / 57 PS | | | | | | Nominal RPM: | 1500 U/min | | | | | | Max. RPM: | 1700 U/min | | | | |
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