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The Horten H.IX, RLM designation Ho 229 (or Gotha Go 229 for extensive re-design work done by Gotha to prepare the aircraft for mass production) was a German prototype fighter/bomber designed by Reimar and Walter Horten to be built by Gothaer Waggonfabrik.
The Horten H.V was a delta-winged, tail-less, twin-engined motor-glider designed and built in the late 1930s and early 1940s by Walter and Reimar Horten in Germany.The H.V aircraft were used for various experimental duties, including: innovative structure, performance, stability and control of flying wing aircraft.
The A model of the H.XVIII was a long, smooth blended wing body.Its six turbojet engines were buried deep in the wing and the exhausts centered on the trailing end. . Resembling the Horten Ho 229 flying wing fighter there were many odd features that distinguished this aircraft; the jettisonable landing gear and the wing made of wood and carbon based glue, are
February 18 – The Horten H.IX V2, the second prototype and first powered prototype of the Horten Ho 229, suffers an engine failure during its third test flight and crashes at Oranienburg, Germany, killing its pilot, Leutnant Erwin Ziller. [47] [48] The third prototype is never completed, and the crash brings the Ho 229 program to an end. [36]
The H.VII was originally allocated the Reichsluftfahrtministerium (RLM) designation 8-226, but was later given the new RLM designation 8-254, so it was known by inference as Horten Ho 226 or Horten Ho 254, though these designations were little used in practice.
Horten intended to test items such as laminar-flow aerofoils and those from other aircraft types, as well as jet engine intakes, at intermediate speeds of up to 300 kilometres per hour (190 mph). [1] It was to be powered by six Argus As 10 176 kilowatts (236 hp) engines driving pusher propellers. [2] Construction was of mixed wood and metal.
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The H.III series was an incremental development of the Horten H.II with reduced sweepback of 23°, span increased to 20 m (65 ft 7 in) and modified lateral controls. The wing trailing edges had three movable surfaces; the innermost was a landing flap, but the outer pair were geared differential elevons with the outer elevon having a large upward deflection and only slight downward movement ...