| 摘要 |
Aircraft having reduced environmental impact. According to the invention, said aircraft comprises at least one engine (10) with at least one propeller (12, 13) carried, at the rear, on the top of said aircraft with the propeller(s) located in vertical alignment with the rear part (2R) of the noise barrier cell and the rear face (16) of the burst zone (14) situated forward of the central part (8C) of the empennage box (8).
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