FIELD: aeronautical engineering; arrangement of main units of aircraft. SUBSTANCE: aircraft has wing 1 and tail unit 4 connected with fuselage 2. Mounted on wing 1 are two engines 5 with pusher propellers. Distance between longitudinal axes of propellers is equal to 1/7 to 1/6 of wing span. EFFECT: enhanced reliability. 2 dwg
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Authors
Dates
1996-09-20—Published
1992-12-30—Filed