摘要 |
<p>The object (10) i.e. firework rocket (10.1), has a body (30) provided with a propellant (31). A hollow tubular guide element (20) stabilizes a trajectory of the object. The guide element is arranged at the body so that a propulsion gas, which arises during igniting the propellant, escapes through the guide element. The guide element and the body are commonly rotationally symmetrically formed. Air openings (23, 24) are evenly distributed around a circumference of the guide element and/or provided on a same height in a flying direction (15) of the object.</p> |