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having a straight trailing edge and a curved leading edge. The cockpit was faired into a large fin and rudder. The undercarriage consisted of a faired central mono-wheel with wing-tip skids. The BICh-3 was flown in Moscow in 1926. It was found to be unstable in initial tests leading to modifications
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https://web.archive.org/web/20091027081510/http://www.geocities.com/unicraftmodels/on/bich3/bich3.htm
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Gunston, Bill. “The Osprey
Encyclopaedia of Russian Aircraft 1875 – 1995”. London, Osprey. 1995.
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that improved the handling sufficiently for it to be cleared as safe to fly.
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Aircraft of comparable role, configuration, and era
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73:Boris Ivanovich Cheranovsky
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231:230 kg (507 lb)
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192:General characteristics
164:Specifications (BICh-3)
454:Chyeranovskii aircraft
336:- archival photographs
172:Gunston, Bill (1995).
322:2012-12-07 at the
176:. London: Osprey.
459:Tailless aircraft
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292:References
264:Horten H.I
217:Wing area:
211:Wingspan:
169:Data from
139:in 1926.
69:Designer
373:aircraft
320:Archived
253:See also
95:retired
428:BICh-26
423:BICh-21
418:BICh-20
413:BICh-18
408:BICh-16
403:BICh-14
398:BICh-11
205:Length:
129:Russian
92:Status
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87:1926
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300:ISBN
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