| 摘要 |
<p>The present invention comes within the sector of infrared decoys for the protection of aircraft. It relates more particularly to a stabilised decoy (4, 21) propelled on a trajectory and having directed infrared emission, comprising a body (22) open on its rear part (24), containing an emissive block (28, 40) of pyrotechnic substance, and an assembly for the ignition of the said block, characterised in that the said body comprises a nose (23) in its front part and has an orifice of constant cross-section in its rear part (24), in that the ignition assembly comprises an ejectable pyromechanical device (6, 26) located at the rear of the said body and an ignition charge (29) located at the front of the said body, and in that the said emissive block (28, 40) has at least one channel and is placed between the ignition charge (29) and the ejectable pyromechanical device (6, 26). <IMAGE></p> |
