To provide a flying object capable of preventing its cargo chamber from becoming unstable in its behavior.

The flying object 1 takes advantage of Coanda effect, and comprises suspensions 4, 5, 6, 7 including a buffer means, damping means, coupling means, and length adjustment means, arranged between the cargo chamber 2 and the wings 3, while the suspensions 4 to 7 are arranged in parallel in the direction in which the flying object 1 proceeds and/or in the right and left directions, with a pair thereof being included.