Infrared signatures of low-flying aircraft and their rear fuselage skin's emissivity optimization

被引:68
作者
Mahulikar, SP [1 ]
Rao, GA [1 ]
Kolhe, PS [1 ]
机构
[1] Indian Inst Technol, Dept Aerosp Engn, Bombay 400076, Maharashtra, India
来源
JOURNAL OF AIRCRAFT | 2006年 / 43卷 / 01期
关键词
D O I
10.2514/1.15365
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper analyzes the main contributors of infrared (IR) signature in a typical aircraft on a low-altitude mission. Various computational models are used to predict IR radiation from the aircraft. The bands within IR spectrum in which aircraft are susceptible to a typical IR-guided surface-to-air and air-to-air missile, for typical cases of tactical relevance, are identified. Lock-on range for aircraft against a typical missile is also computed. The feasibility of a low-altitude mission against a ground-based IR-guided threatis analyzed. The technique of emissivity optimization of aircraft rear fuselage skin, for reducing its infrared signature, is introduced and compared with other IR signature suppression techniques. The effectiveness of this technique in enlarging the safe flight envelope of aircraft, with respect to threat from heat-seeking missiles, for both surface-to-air and air-to-air missiles, is demonstrated. It is found that earthshine reflected off the aircraft surface plays a crucial role in the effectiveness of this technique against a surface-to-air missile (SAM) in 8-12 mu m band.
引用
收藏
页码:226 / 232
页数:7
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