4.7 Article

Performance analysis and design of loitering munitions: A comprehensive technical survey of recent developments

Journal

DEFENCE TECHNOLOGY
Volume 18, Issue 3, Pages 325-343

Publisher

KEAI PUBLISHING LTD
DOI: 10.1016/j.dt.2021.08.010

Keywords

Loitering munition; Unmanned aerial vehicle; Flight performance; Design

Ask authors/readers for more resources

Loitering munitions are increasingly used in armed conflicts. This article presents a database of loitering munitions based on public information, including dimensions, weights, and performance parameters. Statistical trends and aircraft performance theory are used to analyze flight performance and design considerations of new loitering munitions. The preferred design solutions for long-range applications are identified, and case studies are provided to illustrate flight performance capabilities.
Loitering munitions are increasingly used in armed conflicts. An extensive database of loitering muni-tions is developed based on information available in the public domain. This database includes di-mensions, weights, and performance parameters such as flight endurance and communication range. Based upon this dataset, 6 categories of loitering munitions are identified and statistical trends in the form of equations are provided for each category. The statistical trends are supported by aircraft per-formance theory tailored to loitering munitions applications. Altogether, the combination of the data-base, statistical trends and aircraft performance theory can be used to analyse the flight performance and design considerations of new loitering munitions of which only limited non-technical information is available in the public domain such as pictures and news articles. Based on the statistical trends and aircraft performance theory it is concluded that for long range applications, the preferred design solution is the conventional configuration. The cruciform configuration is beneficial in case precision flight path control is of prime importance. The tandem wing configuration combines the benefits of a canister launch and relatively high aspect ratio wings suitable for long range flight. Finally, the delta wing design provides a large internal volume and a high terminal attack airspeed. Two example case studies are included to illustrate the flight performance capabilities of two types of loitering munitions used in the current conflict in Yemen (a long range conventional design and a delta wing configuration).(c) 2021 China Ordnance Society. Publishing services by Elsevier B.V. on behalf of KeAi Communications Co. Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/ licenses/by-nc-nd/4.0/).

Authors

I am an author on this paper
Click your name to claim this paper and add it to your profile.

Reviews

Primary Rating

4.7
Not enough ratings

Secondary Ratings

Novelty
-
Significance
-
Scientific rigor
-
Rate this paper

Recommended

No Data Available
No Data Available