Engineering:Lange Antares
| Antares | |
|---|---|
| |
| Lange Aviation Antares 20E | |
| Role | Open Class and 18 m Class sailplane |
| National origin | Germany |
| Manufacturer | Lange Aviation GmbH |
| First flight | 2003 |
| Number built | 50 as of April 2009 |
The Lange Antares is a glider built by Lange Aviation produced with three different wingspans, 18, 20 and 23 meters. The 20 and 23 meter variants can be equipped with a 42-kW electric motor and SAFT VL 41M lithium-ion batteries.
The EM 42 is a fixed-shaft brushless DC electric motor running at 190-288 V, and drawing up to 160 A, the 42 kW motor can deliver up to 216 N.m of torque over a speed range of 160-1600 RPM with a total efficiency of 90%. Maximum continuous power is 38.5 kW, the motor weighs 29 kg, and the weight of power electronics is 10 kg. The motor turns a two-blade fixed-pitch propeller, LF-P42, constructed of composite materials, having a diameter of two meters.
The battery system consists of two battery packs positioned in the leading edges of both inner wings (72 cells divided into 24 modules containing 3 cells each). The battery life is expected to be 3000 cycles or 20 years. The capacity of the battery is 41 Ah (specific energy 136 Wh/kg and specific peak power 794 W/kg). The batteries can deliver 13 minutes at maximum power and maximum climb speed, and can climb 3,000 meters on one battery charge; in reality, in warm climates, motor and electronics temperature limitations can limit the achievable climb height. The charger is integrated inside the fuselage so when landing elsewhere the pilot merely has to find a (16A) electric outlet socket. The glider has a modem connected to its main computer so that Lange technicians can, in theory, run diagnostics remotely. The same modem allows the pilot remote control & monitoring of the battery charging process.
The undercarriage and engine doors are electro-hydraulically operated. The tailwheel is steerable. The wing has an elliptical planform, with winglets and wing-tip wheels. The glide polar shows excellent high speed performance.
Variants
- Antares 18S - 18 meter wingspan pure glider.
- Antares 18T - 18 meter wingspan glider with Solo 2350 two-stroke gasoline sustainer engine.
- Antares 20E - 20 meter wingspan with 42 kW electric self-launch capable engine.
- Antares 23E - 23 meter wingspan with 42 kW electric self-launch capable engine.
Specifications
Antares 20E
General characteristics
- Crew: one pilot
- Capacity: 100 L water ballast
- Length: 7.40 m (24 ft 3 in)
- Wingspan: 20.00 m (65 ft 7 in)
- Height: 1.64 m (5 ft 5 in)
- Wing area: 12.6 m2 (135.6 sq ft)
- Aspect ratio: 31.7
- Empty weight: 460 kg (1,014 lb)
- Gross weight: 660 kg (1,455 lb)
- Powerplant: 1 × Lange EM 42 , 42 kW (57 hp)
Performance
- Maximum speed: 280 km/h (174 mph, 151 kn)
- Maximum glide ratio: 56
- Rate of climb: 4.4 m/s (866 ft/min)
- Rate of sink: 0.49 m/s (96 ft/min)
Antares 23E
General characteristics
- Crew: one pilot
- Capacity: 250 L water ballast
- Length: 7.48 m (24 ft 6.5 in)
- Wingspan: 23.00 m (75 ft 5.5 in)
- Height: 1.89 m (6 ft 2 in)
- Wing area: 14.75 m2 (158.76 sq ft)
- Aspect ratio: 38.26
- Empty weight: 510 kg (1,124 lb)
- Gross weight: 850 kg (1,873 lb)
- Powerplant: 1 × Lange EM 42 , 42 kW (57 hp)
Performance
- Maximum speed: 280 km/h (174 mph, 151 kn)
- Maximum glide ratio: 60
- Rate of climb: 4.0 m/s (787 ft/min)
- Rate of sink: 0.48 m/s (94.5 ft/min)
See also
Related development
References
- Lange Aviation website
- Specification of Antares 20E
- Specification of Antares 23E
- SAFT VL41M Data sheet
- E1 Antares Type-certificate data sheet
- Lange EA 42 engine Type-certificate data sheet[yes|permanent dead link|dead link}}]
- LF-P42 propeller Type-certificate data sheet[yes|permanent dead link|dead link}}]
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