The Horten H.IV was a German tailless flying wing glider in which the pilot was to lie 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. The H.IV was allocated the RLM ID number 8-251 and by inference Horten Ho 251 though this was little used in practice.
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| - هورتن إتش آي في (ar)
- Horten H IV (de)
- Horten H.IV (en)
- Horten H IV (it)
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| - هورتن إتش آي في(Horten H.IV) كانت طائرة جناح طائر شراعية ألمانية عديمة الذيل، حيث كان على الطيار الاستلقاء في وضعية الانبطاح لتقليل المنطقة الأمامية، وبالتالي السحب. تم تصميمها من قبل ريمار هورتن ووالتر هورتن في غوتينغن. تم بناء أربعة منها بين عامي 1941 و 1943. قامت بالطيران في عدد من المسابقات غير الرسمية في ألمانيا خلال الحرب العالمية الثانية. بعد الحرب، تم نقل نماذج الطيران إلى المملكة المتحدة والولايات المتحدة حيث تم تحقيق العديد من النجاحات في المسابقة. تم تخصيص رقم تعريف (RLM ID) لـ H.IV من (8-251) واستنتاج (Horten Ho 251) على الرغم من أن هذه لم تستخدم كثيرًا في ممارسات الطيران. (ar)
- Die Horten H IV war ein Nurflügel-Versuchssegelflugzeug der Brüder Horten. (de)
- The Horten H.IV was a German tailless flying wing glider in which the pilot was to lie 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. The H.IV was allocated the RLM ID number 8-251 and by inference Horten Ho 251 though this was little used in practice. (en)
- L'Horten H IV, indicato anche come Horten Ho IV dalla convenzione di designazione Reichsluftfahrtministerium (RLM), era un aliante ad alte prestazioni progettato e realizzato in piccola serie dai fratelli Reimar e Walter Horten nei primi anni quaranta. Caratterizzato, come tutta la loro produzione, dalla configurazione tuttala, introduceva anche l'innovazione del posto di pilotaggio in posizione semi-prona per migliorare ulteriormente la del velivolo. (it)
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| sink rate ms
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| span m
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| wing loading kg/m
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| - Reimar and Walter Horten (en)
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| - هورتن إتش آي في(Horten H.IV) كانت طائرة جناح طائر شراعية ألمانية عديمة الذيل، حيث كان على الطيار الاستلقاء في وضعية الانبطاح لتقليل المنطقة الأمامية، وبالتالي السحب. تم تصميمها من قبل ريمار هورتن ووالتر هورتن في غوتينغن. تم بناء أربعة منها بين عامي 1941 و 1943. قامت بالطيران في عدد من المسابقات غير الرسمية في ألمانيا خلال الحرب العالمية الثانية. بعد الحرب، تم نقل نماذج الطيران إلى المملكة المتحدة والولايات المتحدة حيث تم تحقيق العديد من النجاحات في المسابقة. تم تخصيص رقم تعريف (RLM ID) لـ H.IV من (8-251) واستنتاج (Horten Ho 251) على الرغم من أن هذه لم تستخدم كثيرًا في ممارسات الطيران. (ar)
- Die Horten H IV war ein Nurflügel-Versuchssegelflugzeug der Brüder Horten. (de)
- The Horten H.IV was a German tailless flying wing glider in which the pilot was to lie 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. The H.IV was allocated the RLM ID number 8-251 and by inference Horten Ho 251 though this was little used in practice. (en)
- L'Horten H IV, indicato anche come Horten Ho IV dalla convenzione di designazione Reichsluftfahrtministerium (RLM), era un aliante ad alte prestazioni progettato e realizzato in piccola serie dai fratelli Reimar e Walter Horten nei primi anni quaranta. Caratterizzato, come tutta la loro produzione, dalla configurazione tuttala, introduceva anche l'innovazione del posto di pilotaggio in posizione semi-prona per migliorare ulteriormente la del velivolo. Benché indicato come Ho IV, in realtà la convenzione RLM non prevedeva l'uso di numerazione romana dopo il suffisso, difatti la serie numerale assegnata ai velivoli Horten lo indicava come Ho 251. (it)
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| - *Airfoil thickness: 16% T/C ratio
*Sweepback at LE: 20 degrees (en)
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| more performance
| - *Towing speed:
*Landing speed: (en)
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| never exceed speed kmh
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