Projectile from the projectile, - fuselage with wings that

摘要

It is a projectile (10) with vanes (14) is described, which, from the projectile, - hull (12) can be flapped away. Each of the wings (14) has an aerodynamically profiled lead spar (16), a forming the backward direction by a rear spar (22) tensioning element (24) and between the lead spar (16) and the tensioning cable (24) a covering (40) on. The clamp cable (24) is provided with a first end portion (26) with the outer end (28) of the position of the lead spar (16) in the direction of the position of the lead spar (16) - with this at least approximately aligned with -, so that the tensioned tensioning cable (24) in the lead spar (16), no bending force, but rather only a compressive force, so that the lead spar (16) is not subjected to bending and, consequently, with a relatively small profile depth can be designed. The clamp cable (24) is connected with its second end portion (30) to a - in the projectile body (12) provided with a clamping device (32) connected, so that the tensioning cable (24) and the covering (40) in the unfolded state of the wing (14) between the folded open fixed lead spar (16) and the from the tensioned tensioning cable (24) formed on the basis of the spar (22) are permanently tensioned.