A thermally conductive surface (22) of an aerial target (1) is heated using a liquid petroleum gas burner (18) to a sufficient temperature to provide a thermal signature for acquisition by an infrared seeking air defence weapon system. The liquid petroleum gas burner (18) generates a flame which is directed against the thermally conductive surface (22) which then radiates an infrared signature. In the preferred embodiment, the liquid petroleum gas burner (18) is housed within a thermal unit (3) which forms the nose-cone of the aerial target (1).
申请公布号
WO9727446(A1)
申请公布日期
1997.07.31
申请号
WO1997GB00024
申请日期
1997.01.06
申请人
TARGET TECHNOLOGY LIMITED;NEWMAN, PHILIP;RICHARDSON, ALAN