公开(公告)号：US06600165B1

公开(公告)日：2003-07-29

申请号：US09330133

申请日：1999-06-11

Applicant: Pascal Doe ,  Herve Guidetti ,  Gilles Thavot ,  Eric Rantet

Inventor： Pascal Doe ,  Herve Guidetti ,  Gilles Thavot ,  Eric Rantet

IPC: G01J100

CPC classification number: F41J9/08

Abstract: A self-propelled infrared emission aerial target has an aircraft- or a missile-shaped body and a nose, wings and/or control surfaces, a system for feeding fuel and oxidizer to a combustion chamber in which combustion gases are produced and for supplying the combustion gases to a propulsion nozzle, and an infrared radiation emitter. The target has at least one conduit connecting the combustion chamber or propulsion nozzle of the propulsion system to a nose, wing and/or control surface of the target, or to an outside element attached thereto.

Abstract translation: 自推进红外发射空中目标具有飞机或导弹形体以及鼻翼，翼和/或控制表面，用于将燃料和氧化剂供给到其中产生燃烧气体的燃烧室的系统， 燃烧气体到推进喷嘴和红外辐射发射器。 目标具有将推进系统的燃烧室或推进喷嘴连接到靶的鼻，翼和/或控制表面或连接到其上的外部元件的至少一个导管。