AESA radar and IRST against low observable threats
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 27 March 2020
Issue publication date: 27 October 2020
Abstract
Purpose
Modern fighter aircraft using active electronically scanned array (AESA) fire control radars are able to detect and track targets at long ranges, in the order of 50 nautical miles or more. Low observable or stealth technology has contested the radar capabilities, reducing detection/tracking ranges roughly to one-third (or even less, for fighter aircraft radar). Hence, infrared search and track (IRST) systems have been reconsidered as an alternative to the radar. This study aims to explore and compare the capabilities and limitations of these two technologies, AESA radars and IRST systems, as well as their synergy through sensor fusion.
Design/methodology/approach
The AESA radar range is calculated with the help of the radar equation under certain assumptions, taking into account heat dissipation requirements, using the F-16 fighter as a case study. Concerning the IRST sensor, a new model is proposed for the estimation of the detection range, based on the emitted infrared radiation caused by aerodynamic heating.
Findings
The maximum detection range provided by an AESA radar could be restricted because of the increased waste heat which is produced and the relevant constraints concerning the cooling capacity of the carrying aircraft. On the other hand, IRST systems exhibit certain advantages over radars against low observable threats. IRST could be combined with a datalink with the help of data fusion, offering weapons-quality track.
Originality/value
An original approach is provided for the IRST detection range estimation. The AESA/IRST comparison offers valuable insight, while it allows for more efficient planning, at the military acquisition phase, as well as at the tactical level.
Keywords
Citation
Gaitanakis, G.-K., Limnaios, G. and Zikidis, K. (2020), "AESA radar and IRST against low observable threats", Aircraft Engineering and Aerospace Technology, Vol. 92 No. 9, pp. 1421-1428. https://doi.org/10.1108/AEAT-01-2020-0011
Publisher
:Emerald Publishing Limited
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