Engineering:Air Energy AE-1 Silent
From HandWiki
| AE-1 Silent | |
|---|---|
| |
| Role | Ultralight sailplane |
| National origin | Germany |
| Manufacturer | Air Energy |
| First flight | August 1997 |
The Air Energy AE-1 Silent is a German self-launching ultralight sailplane powered by an electric motor. Designed and built by Air Energy, the AE-1 Silent is also marketed by Alisport of Italy, see Alisport Silent 2 Targa.[1][2] It first flew in August 1997.[3]
Design and development
The Silent is a conventional composite monoplane glider with a retractable 13 kW (17 hp) electric motor driving a 1.92m propeller.[4]
The aircraft was originally marketed with a nickel–cadmium battery pack, but in 2005 this was replaced with a lithium polymer battery system that gives three times the range of the early installation.[2]
Specifications
Data from manufacturer[4]
General characteristics
- Crew: 1
- Wingspan: 12 m (39 ft 4 in)
- Wing area: 10.3 m2 (111 sq ft)
- Aspect ratio: 14
- Empty weight: 195 kg (430 lb)
- Gross weight: 300 kg (661 lb)
- Powerplant: 1 × Battery-powered electric motor , 13 kW (17 hp)
Performance
- Maximum speed: 180 km/h (112 mph, 97 kn)
- Service ceiling: 2,000 m (6,560 ft)
- Rate of climb: 2.2 m/s (433 ft/min)
- Rate of sink: 0.78 m/s (154 ft/min)
References
- ↑ "World Directory of Leisure Aviation 2005/2006". World Directory of Light Aviation (Pagefast Ltd, England). 2005. ISSN 1368-485X.
- ↑ 2.0 2.1 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 132. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ↑ "J2mcL Planeurs - Fiche planeur n°". https://www.j2mcl-planeurs.net/dbj2mcl/planeurs-machines/planeur-fiche_0int.php?code=4073.
- ↑ 4.0 4.1 AE-1 Silent
External links
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