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Missile e.g. guided missile, for use with aircraft or combat aircraft, has aero-spike that extends from front face surface, where aero-spike has front body i.e. aero-disk, formed with porous material, whose open pores form flow channels
Missile e.g. guided missile, for use with aircraft or combat aircraft, has aero-spike that extends from front face surface, where aero-spike has front body i.e. aero-disk, formed with porous material, whose open pores form flow channels
The missile (1) has an aero-spike (4) that extends from a front face surface (3), where the aero-spike has a front body i.e. aero-disk (10), formed with a porous material, whose open pores form flow channels. The front body has a front surface that is oriented transverse to a longitudinal axis (11-11) of the missile. A deflecting unit is provided downstream of the channels for outwardly deflecting air flowing through the channels. The aero-spike is formed with a bar, which bears the front body and is supported by a carrier body and a retaining element.
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