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Stanisław Czeszejko
Abstract—In this article the author makes an attempt to characterize the factors which are to be taken into consideration while designing the ground radar component of Air Defense systems, in order to enable them to operate on the modern battlefield. He presents the latest theoretical views on the relationship between the usage of anti-radar weapons and the organizational and technical defense mechanisms which can be deployed against such weapons. In particular the author emphasizes the protection of radars against anti-radiation missiles (ARMs) which present the biggest threat for effective Air Defense systems. He also stresses the need to combine radars into one system which enables the streamlining of their work parameters and thus ensuring their complex usage. The gaining of those capabilities will guarantee that the parameters of the air surveillance radar zone can be defined effectively.
Keywords—anti-radiation missiles, radar, radiolocation, air defense system, survive to operate on the battlefield
I. ANTI-RADIATION MISSILES
SINCE the middle of the 20th century radars have been destroyed by specialized weapons – anti-radiation missiles, homing in on the electromagnetic radiation of the radars. Over the decades the radars have been modified and modernized. New ones have been constructed and different exploitation techniques have been developed. The technical progress of these devices is a never-ending competition. The anti-radiation missiles destroy radars which are elements of the opponent’s air defence system, this in turn allows for the free operating of friendly aircraft within the enemy’s airspace and then also, during combat within the opponent’s territory, their targets are also various objects located there. In the first case, aircrafts carrying these missiles attempt to fulfil the task without entering the striking distance of the ground elements of the enemy’s air defence system (rockets and barrel artillery). Such operations demand proper evaluation of the space striking abilities of the system and to ensure the system is equipped with weapons of the proper strike range needed for destroying the defence system elements. In the second case, the air defence system elements are attacked while crossing the border of their strike range. Also, the weapons systems protecting important objects within the opponent’s territory are eliminated.
While estimating the influence of the anti-radiation missiles’ strike range one cannot neglect the inseparable parameter of the missile flight speed. These two parameters determine the time in which the missile reaches the target after being launched from the plane. Table 1 presents the simplified data concerning the speed, range and flight time of the chosen antiradiation missiles, which shall be discussed in more detail further on. Anti-radiation missiles can be divided roughly according to their range into short range missiles (maximum 100 km), mid-range missiles (maximum 200 km) and long range missiles (over 200 km).
Another important parameter of the anti-radiation missiles is the efficiency of target damage done by the warhead exploding, this is significant for the radar’s survival on the battlefield. In the 1950s the low target accuracy of the anti-radiation missiles was compensated by using warheads of high explosive power, large enough for strategic aircrafts to carry them. During the 1960s three new weight categories of warheads appeared (approximately 150 kg, 86-90 kg and 66 kg); these are still in use with just a few exceptions. In comparison with the former generation of missiles, their higher accuracy and probability of hitting the target allowed for achieving expected striking efficiency in each of these categories. In addition, the distance (altitude) of the fuse from the target was optimized. Such was the situation until the beginning of the 1990s, when the British ALARM missile appeared, whose efficiency is proved by the possibility of attacking a radar with a within 1 meter accuracy (without GPS). For example, the AGM-45 Shrike missile (with approximately a 66 kg warhead) was striking the radars within 15 meters range, and its A version was equipped with high explosives containing 20000 cubic piercing fragments (while hitting the target directly or imprecisely with this missile a high striking effect could be achieved),while the Ch-58USzE missile (with an approximate 150 kg warhead) could hit radars within a range of 20 meters. The target accuracy of the Ch15P and Ch-58USzE missiles is 5-8 meters, of the Ch-31P missile up to 5-7 m, and of the AGM-88 A/B HARM missile the target accuracy is estimated as between 7.3-9 m. Also, for the Ch-58USzE missile the target hitting probability within the range of 20 meters is 0.8. The AGM-88C HARM warhead is equipped with 12845 tungsten cubes (5 mm), able to perforate a 12.7 mm thick soft metal sheet or a 6.35 mm thick armoured plate from a distance of 6 meters, maintaining the missile’s target accuracy. The German ARMIGER missile has quite a small warhead, only 20 kg, and its target accuracy is less than 1 meter (≤ 1 m). Probably the target accuracy of the American AGM-88E AARGM missile is on a similar level to that of the ARMIGER missile (≤ 1 m); since both of them are based on the same construction (AGM-88D HARM) and both represent the same technological advancement level.
But in order to deploy the missile within the efficient strike range it must be equipped with a proper guidance system. Missiles produced in the 1950s and 1960s were homed to the electromagnetic radiation of the radars with support of the inertial guidance system only. The whole process was controlled by a technologically simple autopilot. In the 1970s the dynamic development of miniature transistor-circuit systems began, and they were also employed by the constructors of the anti-radiation missiles homing systems. The following two decades were characterised by the improvement of the existing electronics of the missiles, the aim being the possibility of constructing devices equipped with programmable data bases. They allowed for the comparison of the parameters of detected radars and thus the ability to choose those most dangerous or those which have been pre-defined – as a the specifics of a given combat task demanded. In addition, the contractors increased the possibilities of eliminating jammers, i.e. the sources of purposeful electromagnetic disturbance and thus improved the missiles’ exploitation flexibility.
A conventional anti-radiation missile is homed primarily to the radar’s main lobe emission, but also to the emission of its horizontal side lobes and the back lobes emission – it depends on the distance between the radar and the missile. However, in the case of the older radars the primary target is their horizontal side lobes and back lobes emission of a very high level, which radiate continually. This allows the missile to have uninterrupted tracking of the radar and the passive antiradiation homing receiver does not become saturated. Modern radars with a very low level of the horizontal side lobes and back lobes emissions are a “blinking” target for a missile, and the “blinking” is the result of the intervals in receiving the radar main lobe emission during the turn of its antenna. In such a situation, the on-board systems of missiles without GPS are forced to estimate the radar’s position on the basis of an intermittently received emission. When the turn speed of the antenna is low (long intervals in receiving the emission), the guidance system of the missile is supported by its inertial system, especially during the final phase of flight, which often results with a bigger margin of error (a few meters) in detecting the position of the radar than was assumed beforehand. The error is usually increased to such an extent that in the moment of directly hitting the target the warhead is not set off by a contact fuse but by a proximity fuse. In order to maintain the attack efficiency, the warhead must be equipped with a much stronger explosive.
In 1973, during the Israeli-Arabian Yom Kippur War, conventional anti-radiation missiles of the 1950s’ generation were used. At that time, Egyptian Tu-16 bombers fired 13 KSR-2 and 12 KSR-11 (KSR-2P) missiles from above the Mediterranean towards the targets located on the coast and inside Israeli territory. Most of the missiles (about 20) were intercepted and destroyed by either the air force or the HAWK surface-to-air missiles. 5 of them penetrated through the Israeli air defence system and reached their designated targets. Three radars and one logistic point on the Sinai Peninsula were eliminated. Missiles of the 1970s’ generation were used during the Iraqi-Iranian war (1980–1988) by the Iraqi aircrafts which were targeting Ch-28 missiles towards the radars of the Iranian HAWK systems. Effects of these attacks have not been revealed, unlike the results of the Ch-22MP BURJA missiles which were launched from the Iraqi Tu-22K bombers. Despite numerous launchings towards the HAWK radars, only one missile hit its target. The reason was the poor training of the Iraqi bomber crews, the low efficiency of the guiding system (on the missiles and the deck systems of the bombers), as well as difficulties in efficiently detecting the radars’ position from a long distance. Therefore, later the launchings took place at a distance of 60 km or less and the missiles were carried by the Tu-16 bombers. The targets attacked were mainly located near Teheran: oil refineries and other cities protected by the anti-aircraft system of Iran. The missiles of the 1980s’ generation were used for the first time on 15th April 1986 during the US bombing of Libya (Tripoli and Benghazi), code-named “Operation El Dorado Canyon”. AGM-88A Harm anti-radiation missiles were homed very efficiently eliminating the radars of Libyan air defence system rocket launchers (SA-2 GUIDELINE or S-75 DZWINA, SA-3 GOA or S-125 PECZORA and SA-5 GAMMON or S-200 ANGARA) located around the Gulf of Sidra [1].
In the 1990s the British ALARM missile appeared, introducing some changes in the context of fighting radars. ALARM can be used in the same way as the conventional missiles constructed so far, but in addition it is able to detect and destroy radars independently. It climbs to an altitude of 12000-21000 meters within the task zone [2]. There its engine is turned off, the parachute opens and the missile starts diving slowly, while its passive anti-radiation homing receiver searches for the target – an operating radar. When such is detected, the parachute detaches itself and due to gravity the missile – directed by the guidance system – moves towards the radar. The ALARM missile was created before GPS started to be used in such constructions and its operating method has its reasons. The so called vertical attack of this missile is a result of an assumption that had been made before even the ALARM project appeared. The passive anti-radiation homing receiver of this missile independently homes itself towards the radar emission radiating vertically up, i.e. towards the vertical side lobes. Since most of the radars became able to locate the air objects with high accuracy, the emission level of the horizontal side lobes and back lobes have lowered, in comparison to high emission level of the vertical side lobes. Regardless of the direction of the main lobe emission of the radar, the ALARM passive anti-radiation homing receiver is able to track continuously the fluctuating microwave emission leaking upward from the radar’s antenna.
Guiding to the vertical side lobes (vertical attack at an angle of 90◦) has an additional aspect, namely reducing the influence of emission coming from radiation reflected by the ground objects, which in case of attack at an angle of 20◦40◦ normally widens the margin of error. Taking advantage of it, the ALARM missile is able to attack the target with high accuracy. Moreover, the accuracy is 1 meter, i.e. the explosion should be initiated in the distance of 1 meter from the radar antenna, which increases its most explosive power. The programmable warhead of this missile can have a data base containing information on the general construction of every type of radar, which show, among other details, the place where the antenna is located. This enables the missile to initiate a precise explosion destroying the antenna system or the main electronic systems located in the main blocks of the radar’s board (it depends on what task has been programmed before).It is of special importance in case of eliminating radars whose antennas are raised high, designed for detecting also air objects flying at low altitude. It must be emphasized that the warhead of an anti-radiation missile equipped with smaller explosive exploding very close to the antenna will result in the same destruction level as a warhead with bigger explosive exploding at a greater distance.
Such missiles were used for the first time during the First Gulf War (1990–1991). 121 ALARM missiles were launched from British TORNADO aircraft, which carried out 24 mission aimed only at destroying the air defence system of Iraq and 52 SEAD missions (Suppression of Enemy Air Defences), operating within the opponent’s airspace. In a few cases the launching of the ALARMs of the first experimental series were unsuccessful [2]. In order to eliminate the Iraqi air defence system elements, the coalition forces used also HARM antiradiation missiles. During the “Desert Storm” operation about 2000 of these were launched at the Iraqi radars [3]. A question might be asked as to whether Iraq really had so many air defence radars. However, one can conclude that these missiles were used on many occasions only preventively. Some sources prove that the initiators of such launchings were mainly the pilots of the US Navy (F/A-18 planes), who were using an imprecise warning system – the first version of ALR-67 RWR [4], while the crews of aircrafts designed especially for the SEAD missions, carried out well planned selection, had more time for destroying their targets (it is their main task); they were also better trained and equipped, with much better electronics.
During the First Gulf War ALARM missiles, climbing vertically, were a novelty for many allied pilots. Quite often the missiles speeding upwards (aiming at reaching maximum speed and starting the parachute dive) were mistaken for Iraqi air defence system rockets, which would alarm the battle group unnecessarily, with accounts of such events becoming transformed into various anecdotes.
The analysis of the conflict of the 1990s and experiences resulting from it led to the upgrading of some of the missiles by equipping their guidance systems with additional elements. One of the most important experiences came from the period of NATO operating over the Balkan peninsula. During the NATO air operation called “Deliberate Force” of 1995, American AGM-88 HARM missiles of the first versions were used. In addition the American F-16 aircraft were already then equipped with the Harm Targeting System (HTS), which was used then for the first time in a combat environment. During the 1999 period of this conflict ALARM, AGM-88B HARM and AGM-88C HARM missiles were launched over Serbia and Kosovo, but they were not able to do serious damage to the extremely mobile Yugoslavian air-defence forces. The damages were symbolic and resulted from the too low accuracy of the inertial guiding systems homing the missiles. This provided a strong impulse for the development and later use of GPS in the guidance systems.
In the 1990s, during the Balkan conflict, NATO planes launched altogether 743 HARM missiles, 6 ALARMs and 8 ARMATs towards the radars of the Yugoslavian air defence forces. However, only about 115-130 of the ground targets emitting electromagnetic radiation were attacked, which proves the high efficiency of the Yugoslavian forces’ operations, i.e. the high discipline level concerning the limited time of radars’ radiation (up to 10 seconds) and the high mobility of the forces (constantly changing the positions of the anti-aircraft weapons). The NATO official reports state that the efficiency of the HARM missiles was 3%-6.6%, depending on the operation’s phase [5]. The high efficiency of the Yugoslavian forces was proved by the fact that during the operations the Americans decided to deploy to Italy their experimental Tiger Team from China Lake Weapons Division (USA), an institution testing new weapons. During just 36 days, its pilots tested over 400 HARM missiles, in order to develop new tactics for launching them, allowing for increased efficiency. The effects of their work were instantly transferred to the US Navy units. As a result, immediately more of the attacked objects were destroyed [6].
By the year 2000 the US Air Force and US Marine Corps (USMC) had taken procession of over 19600 AGM-88 Harm missiles of different versions, while by 1997 the German Bundeswehra bought for the Luftwaffe(German Air Force) and Marine flieger (German Naval Air Force) exactly 1000 Harm missiles.
The best known military conflict of the first decade of the 21st century, during which anti-radiation missiles were used, was the Second Gulf War of 2003.The elements of the Iraqi air defence system were being then destroyed by, among others, the HARM missiles – over 400 of them were launched towards all kinds of Iraqi radars [7]. Taking into account the economic situation of Iraq and its low possibilities of recreating its air defence system after the war of 1990-91 and various subsequent air operations (e.g.“Desert Fox”), the number of launched antiradiation missiles might seem too large, especially that they were better developed technologically and also the AGM-88C HARM missiles were already accessible. At that time, the American planes were already equipped with an instrument for launching the anti-radiation missiles for self-protection, and probably this function was used excessively by the crews of the combat planes carrying such missiles. The most recent military conflict, during which the antiradiation missiles were used, was the war in the Southern Ossetia of 2008 (Georgia’s forces vs. combined forces of Southern Ossetia, Abkhazia and Russia). At that time, the basic equipment of the Georgian radar forces was a few ST68U (36D6-M) radars of Soviet production; they were quite difficult to be manoeuvred. In a relatively short time, the Russian air forces managed to eliminate all Georgian radars.
(next page)
Abstract—In this article the author makes an attempt to characterize the factors which are to be taken into consideration while designing the ground radar component of Air Defense systems, in order to enable them to operate on the modern battlefield. He presents the latest theoretical views on the relationship between the usage of anti-radar weapons and the organizational and technical defense mechanisms which can be deployed against such weapons. In particular the author emphasizes the protection of radars against anti-radiation missiles (ARMs) which present the biggest threat for effective Air Defense systems. He also stresses the need to combine radars into one system which enables the streamlining of their work parameters and thus ensuring their complex usage. The gaining of those capabilities will guarantee that the parameters of the air surveillance radar zone can be defined effectively.
Keywords—anti-radiation missiles, radar, radiolocation, air defense system, survive to operate on the battlefield
I. ANTI-RADIATION MISSILES
SINCE the middle of the 20th century radars have been destroyed by specialized weapons – anti-radiation missiles, homing in on the electromagnetic radiation of the radars. Over the decades the radars have been modified and modernized. New ones have been constructed and different exploitation techniques have been developed. The technical progress of these devices is a never-ending competition. The anti-radiation missiles destroy radars which are elements of the opponent’s air defence system, this in turn allows for the free operating of friendly aircraft within the enemy’s airspace and then also, during combat within the opponent’s territory, their targets are also various objects located there. In the first case, aircrafts carrying these missiles attempt to fulfil the task without entering the striking distance of the ground elements of the enemy’s air defence system (rockets and barrel artillery). Such operations demand proper evaluation of the space striking abilities of the system and to ensure the system is equipped with weapons of the proper strike range needed for destroying the defence system elements. In the second case, the air defence system elements are attacked while crossing the border of their strike range. Also, the weapons systems protecting important objects within the opponent’s territory are eliminated.
While estimating the influence of the anti-radiation missiles’ strike range one cannot neglect the inseparable parameter of the missile flight speed. These two parameters determine the time in which the missile reaches the target after being launched from the plane. Table 1 presents the simplified data concerning the speed, range and flight time of the chosen antiradiation missiles, which shall be discussed in more detail further on. Anti-radiation missiles can be divided roughly according to their range into short range missiles (maximum 100 km), mid-range missiles (maximum 200 km) and long range missiles (over 200 km).
Another important parameter of the anti-radiation missiles is the efficiency of target damage done by the warhead exploding, this is significant for the radar’s survival on the battlefield. In the 1950s the low target accuracy of the anti-radiation missiles was compensated by using warheads of high explosive power, large enough for strategic aircrafts to carry them. During the 1960s three new weight categories of warheads appeared (approximately 150 kg, 86-90 kg and 66 kg); these are still in use with just a few exceptions. In comparison with the former generation of missiles, their higher accuracy and probability of hitting the target allowed for achieving expected striking efficiency in each of these categories. In addition, the distance (altitude) of the fuse from the target was optimized. Such was the situation until the beginning of the 1990s, when the British ALARM missile appeared, whose efficiency is proved by the possibility of attacking a radar with a within 1 meter accuracy (without GPS). For example, the AGM-45 Shrike missile (with approximately a 66 kg warhead) was striking the radars within 15 meters range, and its A version was equipped with high explosives containing 20000 cubic piercing fragments (while hitting the target directly or imprecisely with this missile a high striking effect could be achieved),while the Ch-58USzE missile (with an approximate 150 kg warhead) could hit radars within a range of 20 meters. The target accuracy of the Ch15P and Ch-58USzE missiles is 5-8 meters, of the Ch-31P missile up to 5-7 m, and of the AGM-88 A/B HARM missile the target accuracy is estimated as between 7.3-9 m. Also, for the Ch-58USzE missile the target hitting probability within the range of 20 meters is 0.8. The AGM-88C HARM warhead is equipped with 12845 tungsten cubes (5 mm), able to perforate a 12.7 mm thick soft metal sheet or a 6.35 mm thick armoured plate from a distance of 6 meters, maintaining the missile’s target accuracy. The German ARMIGER missile has quite a small warhead, only 20 kg, and its target accuracy is less than 1 meter (≤ 1 m). Probably the target accuracy of the American AGM-88E AARGM missile is on a similar level to that of the ARMIGER missile (≤ 1 m); since both of them are based on the same construction (AGM-88D HARM) and both represent the same technological advancement level.
But in order to deploy the missile within the efficient strike range it must be equipped with a proper guidance system. Missiles produced in the 1950s and 1960s were homed to the electromagnetic radiation of the radars with support of the inertial guidance system only. The whole process was controlled by a technologically simple autopilot. In the 1970s the dynamic development of miniature transistor-circuit systems began, and they were also employed by the constructors of the anti-radiation missiles homing systems. The following two decades were characterised by the improvement of the existing electronics of the missiles, the aim being the possibility of constructing devices equipped with programmable data bases. They allowed for the comparison of the parameters of detected radars and thus the ability to choose those most dangerous or those which have been pre-defined – as a the specifics of a given combat task demanded. In addition, the contractors increased the possibilities of eliminating jammers, i.e. the sources of purposeful electromagnetic disturbance and thus improved the missiles’ exploitation flexibility.
A conventional anti-radiation missile is homed primarily to the radar’s main lobe emission, but also to the emission of its horizontal side lobes and the back lobes emission – it depends on the distance between the radar and the missile. However, in the case of the older radars the primary target is their horizontal side lobes and back lobes emission of a very high level, which radiate continually. This allows the missile to have uninterrupted tracking of the radar and the passive antiradiation homing receiver does not become saturated. Modern radars with a very low level of the horizontal side lobes and back lobes emissions are a “blinking” target for a missile, and the “blinking” is the result of the intervals in receiving the radar main lobe emission during the turn of its antenna. In such a situation, the on-board systems of missiles without GPS are forced to estimate the radar’s position on the basis of an intermittently received emission. When the turn speed of the antenna is low (long intervals in receiving the emission), the guidance system of the missile is supported by its inertial system, especially during the final phase of flight, which often results with a bigger margin of error (a few meters) in detecting the position of the radar than was assumed beforehand. The error is usually increased to such an extent that in the moment of directly hitting the target the warhead is not set off by a contact fuse but by a proximity fuse. In order to maintain the attack efficiency, the warhead must be equipped with a much stronger explosive.
In 1973, during the Israeli-Arabian Yom Kippur War, conventional anti-radiation missiles of the 1950s’ generation were used. At that time, Egyptian Tu-16 bombers fired 13 KSR-2 and 12 KSR-11 (KSR-2P) missiles from above the Mediterranean towards the targets located on the coast and inside Israeli territory. Most of the missiles (about 20) were intercepted and destroyed by either the air force or the HAWK surface-to-air missiles. 5 of them penetrated through the Israeli air defence system and reached their designated targets. Three radars and one logistic point on the Sinai Peninsula were eliminated. Missiles of the 1970s’ generation were used during the Iraqi-Iranian war (1980–1988) by the Iraqi aircrafts which were targeting Ch-28 missiles towards the radars of the Iranian HAWK systems. Effects of these attacks have not been revealed, unlike the results of the Ch-22MP BURJA missiles which were launched from the Iraqi Tu-22K bombers. Despite numerous launchings towards the HAWK radars, only one missile hit its target. The reason was the poor training of the Iraqi bomber crews, the low efficiency of the guiding system (on the missiles and the deck systems of the bombers), as well as difficulties in efficiently detecting the radars’ position from a long distance. Therefore, later the launchings took place at a distance of 60 km or less and the missiles were carried by the Tu-16 bombers. The targets attacked were mainly located near Teheran: oil refineries and other cities protected by the anti-aircraft system of Iran. The missiles of the 1980s’ generation were used for the first time on 15th April 1986 during the US bombing of Libya (Tripoli and Benghazi), code-named “Operation El Dorado Canyon”. AGM-88A Harm anti-radiation missiles were homed very efficiently eliminating the radars of Libyan air defence system rocket launchers (SA-2 GUIDELINE or S-75 DZWINA, SA-3 GOA or S-125 PECZORA and SA-5 GAMMON or S-200 ANGARA) located around the Gulf of Sidra [1].
In the 1990s the British ALARM missile appeared, introducing some changes in the context of fighting radars. ALARM can be used in the same way as the conventional missiles constructed so far, but in addition it is able to detect and destroy radars independently. It climbs to an altitude of 12000-21000 meters within the task zone [2]. There its engine is turned off, the parachute opens and the missile starts diving slowly, while its passive anti-radiation homing receiver searches for the target – an operating radar. When such is detected, the parachute detaches itself and due to gravity the missile – directed by the guidance system – moves towards the radar. The ALARM missile was created before GPS started to be used in such constructions and its operating method has its reasons. The so called vertical attack of this missile is a result of an assumption that had been made before even the ALARM project appeared. The passive anti-radiation homing receiver of this missile independently homes itself towards the radar emission radiating vertically up, i.e. towards the vertical side lobes. Since most of the radars became able to locate the air objects with high accuracy, the emission level of the horizontal side lobes and back lobes have lowered, in comparison to high emission level of the vertical side lobes. Regardless of the direction of the main lobe emission of the radar, the ALARM passive anti-radiation homing receiver is able to track continuously the fluctuating microwave emission leaking upward from the radar’s antenna.
Guiding to the vertical side lobes (vertical attack at an angle of 90◦) has an additional aspect, namely reducing the influence of emission coming from radiation reflected by the ground objects, which in case of attack at an angle of 20◦40◦ normally widens the margin of error. Taking advantage of it, the ALARM missile is able to attack the target with high accuracy. Moreover, the accuracy is 1 meter, i.e. the explosion should be initiated in the distance of 1 meter from the radar antenna, which increases its most explosive power. The programmable warhead of this missile can have a data base containing information on the general construction of every type of radar, which show, among other details, the place where the antenna is located. This enables the missile to initiate a precise explosion destroying the antenna system or the main electronic systems located in the main blocks of the radar’s board (it depends on what task has been programmed before).It is of special importance in case of eliminating radars whose antennas are raised high, designed for detecting also air objects flying at low altitude. It must be emphasized that the warhead of an anti-radiation missile equipped with smaller explosive exploding very close to the antenna will result in the same destruction level as a warhead with bigger explosive exploding at a greater distance.
Such missiles were used for the first time during the First Gulf War (1990–1991). 121 ALARM missiles were launched from British TORNADO aircraft, which carried out 24 mission aimed only at destroying the air defence system of Iraq and 52 SEAD missions (Suppression of Enemy Air Defences), operating within the opponent’s airspace. In a few cases the launching of the ALARMs of the first experimental series were unsuccessful [2]. In order to eliminate the Iraqi air defence system elements, the coalition forces used also HARM antiradiation missiles. During the “Desert Storm” operation about 2000 of these were launched at the Iraqi radars [3]. A question might be asked as to whether Iraq really had so many air defence radars. However, one can conclude that these missiles were used on many occasions only preventively. Some sources prove that the initiators of such launchings were mainly the pilots of the US Navy (F/A-18 planes), who were using an imprecise warning system – the first version of ALR-67 RWR [4], while the crews of aircrafts designed especially for the SEAD missions, carried out well planned selection, had more time for destroying their targets (it is their main task); they were also better trained and equipped, with much better electronics.
During the First Gulf War ALARM missiles, climbing vertically, were a novelty for many allied pilots. Quite often the missiles speeding upwards (aiming at reaching maximum speed and starting the parachute dive) were mistaken for Iraqi air defence system rockets, which would alarm the battle group unnecessarily, with accounts of such events becoming transformed into various anecdotes.
The analysis of the conflict of the 1990s and experiences resulting from it led to the upgrading of some of the missiles by equipping their guidance systems with additional elements. One of the most important experiences came from the period of NATO operating over the Balkan peninsula. During the NATO air operation called “Deliberate Force” of 1995, American AGM-88 HARM missiles of the first versions were used. In addition the American F-16 aircraft were already then equipped with the Harm Targeting System (HTS), which was used then for the first time in a combat environment. During the 1999 period of this conflict ALARM, AGM-88B HARM and AGM-88C HARM missiles were launched over Serbia and Kosovo, but they were not able to do serious damage to the extremely mobile Yugoslavian air-defence forces. The damages were symbolic and resulted from the too low accuracy of the inertial guiding systems homing the missiles. This provided a strong impulse for the development and later use of GPS in the guidance systems.
In the 1990s, during the Balkan conflict, NATO planes launched altogether 743 HARM missiles, 6 ALARMs and 8 ARMATs towards the radars of the Yugoslavian air defence forces. However, only about 115-130 of the ground targets emitting electromagnetic radiation were attacked, which proves the high efficiency of the Yugoslavian forces’ operations, i.e. the high discipline level concerning the limited time of radars’ radiation (up to 10 seconds) and the high mobility of the forces (constantly changing the positions of the anti-aircraft weapons). The NATO official reports state that the efficiency of the HARM missiles was 3%-6.6%, depending on the operation’s phase [5]. The high efficiency of the Yugoslavian forces was proved by the fact that during the operations the Americans decided to deploy to Italy their experimental Tiger Team from China Lake Weapons Division (USA), an institution testing new weapons. During just 36 days, its pilots tested over 400 HARM missiles, in order to develop new tactics for launching them, allowing for increased efficiency. The effects of their work were instantly transferred to the US Navy units. As a result, immediately more of the attacked objects were destroyed [6].
By the year 2000 the US Air Force and US Marine Corps (USMC) had taken procession of over 19600 AGM-88 Harm missiles of different versions, while by 1997 the German Bundeswehra bought for the Luftwaffe(German Air Force) and Marine flieger (German Naval Air Force) exactly 1000 Harm missiles.
The best known military conflict of the first decade of the 21st century, during which anti-radiation missiles were used, was the Second Gulf War of 2003.The elements of the Iraqi air defence system were being then destroyed by, among others, the HARM missiles – over 400 of them were launched towards all kinds of Iraqi radars [7]. Taking into account the economic situation of Iraq and its low possibilities of recreating its air defence system after the war of 1990-91 and various subsequent air operations (e.g.“Desert Fox”), the number of launched antiradiation missiles might seem too large, especially that they were better developed technologically and also the AGM-88C HARM missiles were already accessible. At that time, the American planes were already equipped with an instrument for launching the anti-radiation missiles for self-protection, and probably this function was used excessively by the crews of the combat planes carrying such missiles. The most recent military conflict, during which the antiradiation missiles were used, was the war in the Southern Ossetia of 2008 (Georgia’s forces vs. combined forces of Southern Ossetia, Abkhazia and Russia). At that time, the basic equipment of the Georgian radar forces was a few ST68U (36D6-M) radars of Soviet production; they were quite difficult to be manoeuvred. In a relatively short time, the Russian air forces managed to eliminate all Georgian radars.
(next page)