BICh-7 by B.I.Cheranovsky

A
fter success of the BICh-3 flying wing B.I.Cheranovsky started several other flying wing aircraft projects. One of those was BICh-7, up-scaled single-engined aircraft with open cockpit. It carried two small rudders (without any fins) on the wingtips.
Landing gear was similar to the BICh-3, with single main wheel and three support skids. This time it became a failure. BICh-7 turned very sluggish on takeoff, rudders had little effect.
After few takeoff attempts (not all were successful!) it was rebuilt into the BICh-7A.
PredecessorsModifications

BICh-3

BICh-7A

ReferencesLinks
  • "History of aircraft construction in the USSR" by V.B.Shavrov, Vol.1 p.431;
  • Not found
  • Technical data
    Type BICh-7
    Function Experimental
    Year 1929
    Crew 1
    Engines 1*100hp Bristol-Lucifer
    Length 4.74m
    Wingspan 12.2m
    Wing area 30.0m2
    Empty weight 612kg
    Loaded weight 865kg
    Wing load 29.0kg/m2
    Power load 8.7kg/hp
    Speed at 0M 165km/h
    Landing Speed 70km/h
    Created April 6, 1998
    by Alexandre Savine
    Back to
    Main Gate