1937, single-seat performance glider, cantilevered gull-wings, retractable landing-gear, all-moving-tail, dive air-brakes, all-wood
Glider
Akaflieg Berlin B 3 Charlotte II
1923, single-seat glider, air brakes, one skid, otherwise like B 1
Akaflieg Berlin B 2 Teufelchen
1923, single-seat glider, cantilever shoulder-wing, all-wood
Akaflieg Berlin B 1 Charlotte
1922, single-seat glider, tailless, shoulder-wing, two skids, all-wood
Akaflieg Berlin
2008:
Straffe des 17. Juni 135
Berlin 10623
Germany
Akademische Fliegergruppe Hannover AFH-24
Designed by Akaflieg Hannover of Germany.
Wing span: 15m
Wing area: 10.27sq.m
Empty Weight: 245kg
Gross Weight: 500kg
Wing Load: 46.7kg/sq.m
Aspect ratio: 21.91
Airfoil: HQ
Structure: GFRP
Seats: 1
Number built: 1
Akademische Fliegergruppe Hannover
Welfengarten 1a
30167
Hanover
Germany
Airsport s.r.o Sonata
Ultralight Motor Glider with retractable prop.
Stall: 30 kt / 34 mph / 55 kmh
Cruise: 49 kt / 56 mph / 90 kmh
VNE: 97 kt / 112 mph / 180 kmh
Empty Weight: 278 kg / 613 lbs
MTOW Weight: 450 kg / 992 lbs
Climb Ratio: 400 ft/min / 2 m/s
Glide Ratio: 1:36
Airsport s.r.o
Airsport sro is a privately held company Czech aircraft manufacturer based in Zbraslavice. The company specializes in the design and manufacture of microlight aircraft and motorgliders in the form of kits for amateur construction and ready-to-fly aircraft for the European Fédération Aéronautique Internationale microlight category.
The company had three designs in production as of 2015, all constructed from composite materials. The Airsport Sonet is a light touring aircraft derived from the Airsport Sonata motorglider. The Airsport Song is a single-seat motorglider, with a twin-boom and inverted V-tail layout.
Airspeed AS.54
The Airspeed AS.54 was a two-seat training glider designed to A.M. Spec. TX3/43, to train pilots to fly large transport gliders. Wood and ply construction, it was not built.
The undercarriage was self-jettisoning mainwheel and central skid. Dive brakes and split trailing-edge flaps were designed and water ballast was in the fuselage.
The wing was three-piece, with a centre-section of 4.57 m / 15 ft span, stut braced.
Wingspan: 10.97 m / 36 ft 0 in
Wing area: 14.59 sq.m / 157 sq.ft
Length: 8.18 m / 26 ft 10 in
AUW: 853 kg / 1880 lb
Wing loading: 58.6 kg/s.m / 12 lb/sq.ft
Max speed: 322 kph / 200 mph
Stall: 79 kph / 49 mph
