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A loitering munition (also known as a suicide drone or kamikaze drone) is a weapon system category in which the munition loiters around the target area for some time, searches for targets, and attacks once a target is located. Loitering munitions enable faster reaction times against concealed or hidden targets that emerge for short periods without placing high-value platforms close to the target area, and also allow more selective targeting as the actual attack mission can be aborted.
Loitering munitions fit in the niche between cruise missiles and unmanned combat aerial vehicles (UCAVs) sharing characteristics with both. They differ from cruise missiles in that they are designed to loiter for a relatively long time around the target area, and from UCAVs in that a loitering munition is intended to be expended in an attack and has a built-in warhead.
Loitering weapons first emerged in the 1980s for use in the Suppression of Enemy Air Defenses (SEAD) role against surface-to-air missiles (SAMs), and were deployed for the SEAD role in a number of military forces in the 1990s. Starting in the 2000s, loitering weapons have been developed for additional roles ranging from relatively long-range strikes and fire support down to tactical, very short range battlefield systems that fit in a backpack.
Loitering munitions have proliferated into use by at least 14 countries, with several different types in use as of 2017. The rising proliferation and the ability to use some systems as lethal autonomous weapons coupled with ethical concerns over such use have led to research and discussion by International humanitarian law scholars and activists.
Initially, loitering munitions were not referred to as such but rather as suicide UAVs or loitering missiles. Different sources point at different projects as originating the weapon category. The early 1980s initial Israeli Delilah variants or the failed US AGM-136 Tacit Rainbow program are mentioned by some sources. Alternatively, the late 1980s IAI Harpy which was widely exported is considered by some as the first loitering munition system.
Early projects did not use the "loitering munition" nomenclature which emerged at a much later date, and used existing terminology at the time. For instance the AGM-136 Tacit Rainbow was described as follows in a 1988 Air Force Magazine article:
the Tacit Rainbow unmanned jet aircraft being developed by Northrop to loiter on high and then swoop down on enemy radars could be called a UAV, a cruise missile, or even a standoff weapon. But it is most definitely not an RPV.
The response to the first generation of fixed installation surface-to-air missiles (SAMs) such as SA-2 and SA-3 was the development of the anti-radiation missile such as AGM-45 Shrike and other means to attack fixed SAM installations, as well as developing SEAD doctrines. The Soviet counter-response was the use of mobile SAMs such as SA-6 with intermittent use of radar. Thus, the SAM battery was only visible for a small period of time, during which it was also a significant threat to high-value Wild Weasel fighters. In 1982 Operation Mole Cricket 19 various means including UAVs and air-launched Samson decoys were used over suspected SAM areas to saturate enemy SAMs and to bait them to activate their radar systems, which were then attacked by anti-radiation missiles.
In the 1980s, a number of programs, such as the IAI Harpy or the AGM-136 Tacit Rainbow, integrated anti-radiation sensors into a drone or missile air frames coupled with command and control and loitering capabilities. This allowed the attacking force to place relatively cheap munitions in place over suspected SAM sites, and to attack promptly the moment the SAM battery is visible. This integrated the use of a drone as a baiting decoy with the attack role into one small and relatively cheap platform in comparison to the alternative wild weasel jet fighter.
Starting in the 2000s, loitering weapons have been developed for additional roles beyond the initial SEAD role ranging from relatively long-range strikes and fire support down to tactical, very short-range battlefield use such as the AeroVironment Switchblade which is deployed at the platoon level and fits in a backpack. A documented use of loitering munitions was in 2016 Nagorno-Karabakh clashes in which an IAI Harop was used against a bus functioning as a troop transport.
Loitering munitions may be as simple as an unmanned aerial vehicle (UAV) with attached explosives that is sent on a potential kamikaze mission, and may even be constructed with off the shelf commercial quadcopters with strapped on explosives.
Purpose built munitions are more elaborate in flight and control capabilities, warhead size and design, and on-board sensors for locating targets. Some loitering munitions use a human operator to locate targets whereas others, such as IAI Harop, can function autonomously searching and launching attacks without human intervention.
Some loitering munitions may return and be recovered by the operator if they are unused in an attack and have enough fuel; in particular this is characteristic of UAVs with a secondary suicide mission. Other systems, such as Delilah or IAI Harop, don't have a recovery option and are self-destructed in mission aborts.
The following table compares similar size-class cruise missiles, loitering munitions, and UCAVS:
|Characteristic||Cruise missile||Loitering munition||UCAV|
|Cost appropriate for expendable one-time use||Yes||Yes||No, but high cost allows for higher-quality platform|
|Recovery possible after launch||No||Usually no||Yes, typical mission profile is round-trip|
|Stealthy final dive to target||Usually yes||Usually yes||Usually no|
|Loitering||No or limited||Yes||Usually yes|
|Sensors for target acquisition||Limited||Yes||Usually yes|
|command and control during flight||Usually limited||Yes||Yes|
|Range||Longer, optimized for constant speed flight||Shorter||Shorter, even shorter for typical round-trip mission|
|Speed||Typically higher||Typically lower||Depends on role|
|Range||1,600 km||1,000 km||1,100 km|
|Max speed||high sub-sonic, 880 km/h||190 km/h||217 km/h|
|Flight endurance||c. 2 hours||6 hours||24 hours|
|Engine||3.1 kilonewtons (700 lbf) F107-WR-402 turbofan engine||37 hp Wankel engine||115 hp Rotax 914F|
|Loaded system weight||1,588 kg||135 kg||1,020 kg|
|Payload||450 kg warhead||23 kg warhead||2 × AGM-114 Hellfire or 6 × AGM-176 Griffin air-to-surface missiles|
|Length||6.25 m||2.5 m||8.22 m|
|Wingspan||2.67 m ||3.0 m ||16.8 m |
Whereas some cruise missiles, such as the block IV Tomahawk, have the ability to loiter and have some sensory and remote control features, their primary mission is typically strike and not target acquisition. Cruise missiles, as their name implies, are optimized for long-range flight at constant speed both in terms of propulsion systems and wings or lifting body design. They are often unable to loiter at slow fuel-efficient speeds which significantly reduces potential loiter time even when the missile has some loiter capabilities.
Conversely almost any UAV could be piloted to crash onto a target in a suicide attack and most could be fitted with an improvised explosive warhead. However the primary use of a UAV or UCAV would be for recoverable flight operations carrying reconnaissance equipment and/or munitions. While many UAV designs are explicitly designed with loitering in mind, they are not optimized for a diving attack often lacking forward facing cameras, lacking in control response-speed which is unneeded in regular UAV flight, and are noisy when diving at the target potentially providing warning to the target. UAV's, being designed as multi-use platforms, often have a unit cost that is not appropriate for regular one-time expendable mission use.
The primary mission of a loitering munition is reaching the suspected target area, target acquisition during a loitering phase, followed by a suicide strike, and the munition is optimized in this regard in terms of characteristics (e.g. very short engine life time, silence in strike phase, speed of strike dive, optimization toward loitering time instead of range/speed) and unit cost (appropriate for a one-off strike mission).
Loitering munitions that are capable of making autonomous attack decisions (man out of the loop) raise moral, ethical, and international humanitarian law concerns because a human being is not involved in making the actual decision to attack and potentially kill humans. Whereas some guided munitions may lock-on after launch or may be sensor fuzed, their flight time is typically limited and a human launches them at an area where enemy activity is strongly suspected. An autonomous loitering munition, on the other hand, may be launched at an area where enemy activity is only probable, and loiter searching autonomously for targets for potentially hours following the initial launch decision. The IAI Harpy and IAI Harop are frequently cited in the relevant literature as they set a precedent for an aerial system (though not necessarily a precedent when comparing to a modern naval mine) in terms of length and quality of autonomous function, in relation to a cruise missile for example.
As of 2017, loitering munitions are in use in several countries, including: