Puneet Varma (Editor)

Horten H.IV

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Top speed
  
200 km/h

Length
  
3.81 m

Wingspan
  
20 m

Horten H.IV FileHorten H IV Deutsches Museumjpg Wikimedia Commons

Pauls horten h iv maiden flight long mynd


The Horten H.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. During World War II, these aircraft participated in a series of unofficial competitions in Germany. Following the war, the operational models were transported to the United Kingdom and the United States, where they achieved several successes in contests.

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Specifications

Data from

General characteristics

Horten H.IV Horten HoIV Aircraft

  • Crew: 1
  • Length: 3.81 m (12 ft 6 in)
  • Wingspan: 20.3 m (66 ft 7 in)
  • Wing area: 18.9 m2 (203 sq ft)
  • Aspect ratio: 21.8
  • Empty weight: 250 kg (551 lb)
  • Gross weight: 330 kg (728 lb)
  • Aerofoil thickness: 16% T/C ratio
  • Sweepback at LE: 20 degrees
  • Performance

    Horten H.IV hoiv

  • Never exceed speed: 200 km/h (124 mph; 108 kn)
  • Maximum glide ratio: 32 at 73 km/h (45 mph) and 17.5 kg/m² (3.6 lb/sq ft)
  • Rate of sink: 0.5 m/s (98 ft/min) at 60 km/h (37 mph) and 17.5 kg/m² (3.6 lb/sq ft)
  • Wing loading: 17.5 kg/m2 (3.6 lb/sq ft)
  • Towing speed: 55 km/h (34 mph)
  • Landing speed: 55 km/h (34 mph)

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    References

    Horten H.IV Wikipedia