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Horten H.IV
From PlaneSpottingWorld, for aviation fans everywhere
The Horten Ho IV was a German tailless flying wing glider in which the pilot lay in a prone position to reduce the frontal area, and hence drag. It was designed by Reimar and Walter Horten in Göttingen. Four were built between 1941 and 1943. They were flown in a number of unofficial competitions in Germany during World War II. After the war the flying examples were transported to the United Kingdom and the United States where several contest successes were achieved.
Specifications
General characteristics
- Crew: 1
- Length: 3.81 m (12 ft 6 in)
- Wingspan: 20.3 m (66 ft 7 in)
- Height: ()
- Airfoil: 21.8
- Empty weight: 246 kg (541 lb)
- Loaded weight: 349 kg (768 lb)
- * Minimum sink rate: 0.55 m/s at 55 km/h (1.8 ft/sec at 34.2mph)
- Best glide ratio: 32 at 73 km/h (45.3mph)
Performance
- Maximum speed: 200 km/h (108 kts, 124 mph)
External links
See also
Related lists
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General | Timeline of aviation · Aircraft · Aircraft manufacturers · Aircraft engines · Aircraft engine manufacturers · Airports · Airlines |
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Records | Flight airspeed record · Flight distance record · Flight altitude record · Flight endurance record · Most produced aircraft |
Lists relating to aviation | |
---|---|
General | Timeline of aviation · Aircraft · Aircraft manufacturers · Aircraft engines · Aircraft engine manufacturers · Airports · Airlines |
Military | Air forces · Aircraft weapons · Missiles · Unmanned aerial vehicles (UAVs) · Experimental aircraft |
Notable incidents and accidents | Military aviation · Airliners · General aviation · Famous aviation-related deaths |
Records | Flight airspeed record · Flight distance record · Flight altitude record · Flight endurance record · Most produced aircraft |
This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Horten H.IV". |