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70-588: The A-350 was introduced during the 1960s with mechanically steered semi-active radar guidance . It contained a high-yield nuclear warhead , comparable to the U.S. Nike Zeus . The A-350R (NATO reporting name ABM-1B ) was introduced with the advanced A-35M missile system and became operational during 1978. This system was tested at the Sary Shagan Launch Facility with five test flights during 1971, 1976, and 1977, with two more tests during 1993 and 1999. The next generation of missiles, introduced with

140-671: A combination of any of those three warhead types) is typically used in the attempt to disable or destroy the target aircraft. Warheads are typically detonated by a proximity fuze or by an impact fuze if it scores a direct hit. Less commonly, nuclear warheads have been mounted on a small number of air-to-air missile types (such as the AIM-26 Falcon ) although these are not known to have ever been used in combat. Guided missiles operate by detecting their target (usually by either radar or infrared methods, although rarely others such as laser guidance or optical tracking ), and then "homing" in on

210-451: A cone shape as the distance from the attacking aircraft increases. This will result in less accuracy for the missile because the beam may actually be larger than the target aircraft when the missile arrives. The missile could be securely within the beam but still not be close enough to destroy the target. Infrared guided (IR) missiles home on the heat produced by an aircraft. Early infra-red detectors had poor sensitivity, so could only track

280-484: A fault prevents datalink self-destruct signals when a missile is heading in the wrong direction. Most coastlines are heavily populated, so this risk exists at test centers for sea-based systems that are near the coastlines: The combat record of U.S. SARH missiles was unimpressive during the Vietnam War . USAF and US Navy fighters armed with AIM-7 Sparrow attained a success rate of barely 10%, which tended to amplify

350-605: A more powerful motor that allows the missile to maneuver against crossing targets and launch at greater ranges, gives the launching aircraft improved tactical freedom. Other members of the 4th generation use focal plane arrays to offer greatly improved scanning and countermeasures resistance (especially against flares). These missiles are also much more agile, some by employing thrust vectoring (typically gimballed thrust ). The latest generation of short-range missiles again defined by advances in seeker technologies, this time electro-optical imaging infrared (IIR) seekers that allow

420-576: A narrow (30-degree) field of view and required the attacker to position himself behind the target ( rear aspect engagement ). This meant that the target aircraft only had to perform a slight turn to move outside the missile seeker's field of view and cause the missile to lose track of the target ("break lock"). The second-generation of short-range missiles utilized more effective seekers that were better cooled than its predecessors while being typically "uncaged"; resulting in improved sensitivity to heat signatures, an increase in field of view as well as allowing

490-582: A number of times, varying the locations, sectors or quadrants, and number of launchers. The system finalized at 8 sites with total of 64 launchers, with 4 major radar centers completed. With on-going advancements in the ABM system, radars, missile and warheads, the evolution of the A-35 became the A-35M. The "M" for modernization, was brought on through the advanced developments at 10 different Soviet institutes. One primary upgrade

560-455: A period of growth and modifications. Configurations included an improved A-350Zh with tests during 1973. Eventually, the design changed again with radiation-hardened cases and became the A-350R for Phase 2 deployment in 1974. The construction of the A-35 system began during 1962 with 16 primary sites including command post, radar installations and firing complexes for 8–16 missile launchers. Some of

630-411: A rocket of some type and the control actuation system or CAS. Dual-thrust solid-fuel rockets are common, but some longer-range missiles use liquid-fuel motors that can "throttle" to extend their range and preserve fuel for energy-intensive final maneuvering. Some solid-fuelled missiles mimic this technique with a second rocket motor which burns during the terminal homing phase. There are missiles, such as

700-407: A specified range. Towed decoys which closely mimic engine heat and infra-red jammers can also be used. Some large aircraft and many combat helicopters make use of so-called "hot brick" infra-red jammers, typically mounted near the engines. Current research is developing laser devices which can spoof or destroy the guidance systems of infra-red guided missiles. See Infrared countermeasure . Start of

770-558: A target from various angles, not just from behind, where the heat signature from the engines is strongest. Other types rely on radar guidance (either on-board or "painted" by the launching aircraft). In 1999 R-73 missile were adapted by Serb forces for surface to air missiles. The Houthi movement Missile Research and Development Centre and the Missile Force have tried to fire R-27/R-60/R-73/R-77 against Saudi aircraft. Using stockpiles of missiles from Yemeni Air Force stocks. The issue for

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840-460: A wider pattern. Modern SARH systems use continuous-wave radar (CW radar) for guidance. Even though most modern fighter radars are pulse Doppler sets, most have a CW function to guide radar missiles. A few Soviet aircraft, such as some versions of the MiG-23 and MiG-27 , used an auxiliary guidance pod or aerial to provide a CW signal. The Vympel R-33 AA missile for MiG-31 interceptor uses SARH as

910-414: Is a monopulse radar receiver that produces angle error measurements using that fixed position. Flight path is controlled by producing navigation input to the steering system (tail fins or gimbaled rocket) using angle errors produced by the antenna. This steers the body of the missile to hold the target near the centerline of the antenna while the antenna is held in a fixed position. The offset angle geometry

980-446: Is a commonly used modern missile guidance methodology, used in multiple missile systems, such as: Air-to-air missile An air-to-air missile ( AAM ) is a missile fired from an aircraft for the purpose of destroying another aircraft (including unmanned aircraft such as cruise missiles ). AAMs are typically powered by one or more rocket motors , usually solid fueled but sometimes liquid fueled . Ramjet engines, as used on

1050-456: Is called "off- boresight " launch. For example, the Russian Su-27 is equipped with an infra-red search and track (IRST) system with laser rangefinder for its HMS-aimed missiles. A recent advancement in missile guidance is electro-optical imaging. The Israeli Python-5 has an electro-optical seeker that scans designated area for targets via optical imaging. Once a target is acquired,

1120-667: Is determined by flight dynamics using missile speed, target speed, and separation distance. Techniques are nearly identical using jamming signals , optical guidance video, and infra-red radiation for homing. Maximum range is increased in SARH systems using navigation data in the homing vehicle to increase the travel distance before antenna tracking is needed for terminal guidance. Navigation relies on acceleration data , gyroscopic data , and global positioning data . This maximizes distance by minimizing corrective maneuvers that waste flight energy. Contrast this with beam riding systems, like

1190-577: Is possible for the system to take missiles straight from an aircraft. After a live-fire test occurred in September 2020 off the coasts of Florida, during which it successfully engaged a simulated cruise missile, in 2022 NASAMS was deployed to Ukraine, where for the first time this missile system was used in real combat conditions, and, according to Ukrainian government, was able to shot down more than 100 aerial targets. A conventional explosive blast warhead, fragmentation warhead, or continuous rod warhead (or

1260-589: Is still a limitation to some degree) and could be distracted by the sun, a reflection of the sun off of a cloud or ground object, or any other "hot" object within its view. More modern infra-red guided missiles can detect the heat of an aircraft's skin, warmed by the friction of airflow, in addition to the fainter heat signature of the engine when the aircraft is seen from the side or head-on. This, combined with greater maneuverability, gives them an " all-aspect " capability, and an attacking aircraft no longer had to be behind its target to fire. Although launching from behind

1330-489: Is subject to a minimum range, before which it cannot maneuver effectively. In order to maneuver sufficiently from a poor launch angle at short ranges to hit its target, some missiles use thrust vectoring , which allow the missile to start turning "off the rail", before its motor has accelerated it up to high enough speeds for its small aerodynamic surfaces to be useful. Short-range air-to-air missiles (SRAAMs), typically used in " dogfighting " or close range air combat compare to

1400-414: Is that it enables a " fire-and-forget " mode of attack, where the attacking aircraft is free to pursue other targets or escape the area after launching the missile. Semi-active radar homing (SARH) guided missiles are simpler and more common. They function by detecting radar energy reflected from the target. The radar energy is emitted from the launching aircraft's own radar system. However, this means that

1470-426: Is that since almost all detection and tracking systems consist of a radar system, duplicating this hardware on the missile itself is redundant. The weight of a transmitter reduces the range of any flying object, so passive systems have greater reach. In addition, the resolution of a radar is strongly related to the physical size of the antenna, and in the small nose cone of a missile there isn't enough room to provide

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1540-512: Is the "home on jam" mode which, when installed, allows a radar-guided missile to home in on the jammer of the target aircraft if the primary seeker is jammed by the electronic countermeasures of the target aircraft. Air-to-air missiles are typically long, thin cylinders in order to reduce their cross section and thus minimize drag at the high speeds at which they travel. Missiles are divided into five primary systems (moving forward to aft): seeker, guidance, warhead, motor, and control actuation. At

1610-528: The R-60M or the Python-3 . The R-73 (missile) ( AA-11 Archer ) entered service in 1985 and marked a new generation of dogfight missile. It had a wider field of view and could be cued onto a target using a helmet mounted sight . This allowed it to be launched at targets that would otherwise not be seen by older generation missiles that generally stared forward while waiting to be launched. This capability, combined with

1680-517: The A-135 ABM System , were the 53T6 (1970s) and the 51T6 (1980s). The A-350 was a three-stage solid-fueled design with a range of over 300 kilometers. It was improved with a restartable liquid-fueled third stage. This gave a much improved post-launch and re-targeting capabilities. The A-350 are launched from above-ground launchers. The missile design was done by MKB Fakel 's Chief Designer Petr Grushin . The system had multiple radars during

1750-665: The ASRAAM and Sea Ceptor . The air-to-air missile grew out of the unguided air-to-air rockets used during the First World War . Le Prieur rockets were sometimes attached to the struts of biplanes and fired electrically, usually against observation balloons , by such early pilots as Albert Ball and A. M. Walters. Facing the Allied air superiority, Germany in World War II invested limited effort into missile research, initially adapting

1820-577: The Dunay-3U omni-direction 360-degree search radar, designed by V. P. Sosulnikov and A. N. Musatov, respectively. A more advanced system of radars were included, the Don-2N System; consisting of the 6000 km long-range early warning radars Don-2N and Dnestr, (NATO code names Pill Box and Hen House ), and the 2800 km short-range target acquisition radars Dunay-3M and Dunay-3U (NATO codenames Dog House and Cat House ). The A-350 developed through

1890-715: The Meteor , are emerging as propulsion that will enable future medium- to long-range missiles to maintain higher average speed across their engagement envelope. Air-to-air missiles are broadly put in two groups. Those designed to engage opposing aircraft at ranges of around 30 km to 40 km maximum are known as short-range or "within visual range" missiles (SRAAMs or WVRAAMs) and are sometimes called " dogfight " missiles because they are designed to optimize their agility rather than range. Most use infrared guidance and are called heat-seeking missiles. In contrast, medium- or long-range missiles (MRAAMs or LRAAMs), which both fall under

1960-539: The RIM-8 Talos , in which the radar is pointed at the target and the missile keeps itself centered in the beam by listening to the signal at the rear of the missile body. In the SARH system the missile listens for the reflected signal at the nose, and is still responsible for providing some sort of "lead" guidance. The disadvantages of beam riding are twofold: One is that a radar signal is "fan shaped", growing larger, and therefore less accurate, with distance. This means that

2030-446: The beyond-visual-range missiles . Most of the short-range air-to-air missiles are infrared guided . Those missiles usually classified into five "generations" according to the historical technological advances. Most of these advances were in infrared seeker technology (later combined with digital signal processing ). Early short-range missiles such as the early Sidewinders and K-13 (missile) ( AA-2 Atoll ) had infrared seekers with

2100-492: The 21st century missiles such as the ASRAAM use an " imaging infrared " seeker which "sees" the target (much like a digital video camera), and can distinguish between an aircraft and a point heat source such as a flare. They also feature a very wide detection angle, so the attacking aircraft does not have to be pointing straight at the target for the missile to lock on. The pilot can use a helmet mounted sight (HMS) and target another aircraft by looking at it, and then firing. This

2170-488: The MBDA Meteor, that "breathe" air (using a ramjet , similar to a jet engine) in order to extend their range. Modern missiles use "low-smoke" motors – early missiles produced thick smoke trails, which were easily seen by the crew of the target aircraft alerting them to the attack and helping them determine how to evade it. The CAS is typically an electro-mechanical, servo control actuation system, which takes input from

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2240-530: The R-27 and R-77 is the lack of a radar to support their guidance to the target. However the R-73 and R-60 are infra-red heat seeking missiles. They only require, power, liquid nitrogen "to cool the seeker head" and a pylon to launch the missile. These missiles have been paired with a "US made FLIR Systems ULTRA 8500 turrets". Only one near miss has been verified and that was a R-27T fired at Royal Saudi Air Force F-15SA. However

2310-628: The Sparrow at beyond visual range . Similar performance has been achieved with the sea-launched RIM-7 Sea Sparrow . Soviet systems using SARH have achieved a number of notable successes, notably in the Yom Kippur War , where 2K12 Kub (NATO name SA-6) tactical SAM systems were able to effectively deny airspace to the Israeli Air Force . A 2K12 also shot down a U.S. F-16 in the Bosnian War. SARH

2380-572: The US that early F-4 variants were armed only with missiles in the 1960s. High casualty rates during the Vietnam War caused the US to reintroduce autocannon and traditional dogfighting tactics but the missile remains the primary weapon in air combat. In the Falklands War British Harriers , using AIM-9L missiles were able to defeat faster Argentinian opponents. Since the late 20th century all-aspect heat-seeking designs can lock-on to

2450-527: The USN's AIM-7 Sparrow and AIM-9 Sidewinder . Post-war research led the Royal Air Force to introduce Fairey Fireflash into service in 1957 but their results were unsuccessful. The Soviet Air Force introduced its K-5 into service in 1957. As missile systems have continued to advance, modern air warfare consists almost entirely of missile firing. The use of beyond-visual-range combat became so pervasive in

2520-683: The anti-radiation missile (ARM) design, pioneered during Vietnam and used to home in against emitting surface-to-air missile (SAM) sites, to an air intercept weapon. Current air-to-air passive anti-radiation missile development is thought to be a countermeasure to airborne early warning and control (AEW&C – also known as AEW or AWACS) aircraft which typically mount powerful search radars. Due to their dependence on target aircraft radar emissions, when used against fighter aircraft passive anti-radiation missiles are primarily limited to forward-aspect intercept geometry. For examples, see Vympel R-27 and Brazo . Another aspect of passive anti-radiation homing

2590-657: The attack radar to illuminate the target during part or all of the missile interception itself. Radar guidance is normally used for medium- or long-range missiles, where the infra-red signature of the target would be too faint for an infra-red detector to track. There are three major types of radar-guided missile – active, semi-active, and passive. Radar-guided missiles can be countered by rapid maneuvering (which may result in them "breaking lock", or may cause them to overshoot), deploying chaff or using electronic counter-measures . Active radar (AR)-guided missiles carry their own radar system to detect and track their target. However,

2660-530: The beam riding system is not accurate at long ranges, while SARH is largely independent of range and grows more accurate as it approaches the target, or the source of the reflected signal it listens for. Reduced accuracy means the missile must use a very large warhead to be effective (i.e.: nuclear). Another requirement is that a beam riding system must accurately track the target at high speeds, typically requiring one radar for tracking and another "tighter" beam for guidance. The SARH system needs only one radar set to

2730-424: The category of beyond-visual-range missiles (BVRAAMs), tend to rely upon radar guidance, of which there are many forms. Some modern ones use inertial guidance and/or "mid-course updates" to get the missile close enough to use an active homing sensor. The concepts of air-to-air missiles and surface-to-air missiles are closely related, and in some cases versions of the same weapon may be used for both roles, such as

2800-699: The different phases including the Don-2N radar and Dnestr radar early warning systems, and the Dunay radar target acquisition systems. The A-35 with radar was designed by Chief Designer K. B. Kisunko. The idea for this system was to protect Moscow from nuclear attack by the United States. The Soviet government began studies during 1958 with preliminary designs from General Designer K. B. Kisunko . Further designs and development were moved to TsNPO Vympel . Radar systems were tested with Duna-3 single direction search radar and

2870-545: The drawback is that these missiles are intended to be fired from one jet fighter against another. So the motors and fuel load are smaller than a purpose built surface to air missile. On the Western side, the Norwegian-American made NASAMS air defense system has been developed for using AIM-9 Sidewinder , IRIS-T and AMRAAM air-to-air missiles to intercept targets. None of these missiles require modifications and hence it

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2940-420: The effect of removing the gun on most F-4 Phantoms , which carried 4 Sparrows. While some of the failures were attributable to mechanical failure of 1960s-era electronics, which could be disturbed by pulling a cart over uneven pavement, or pilot error; the intrinsic accuracy of these weapons was low relative to Sidewinder and guns. Since Desert Storm , most F-15 Eagle combat victories have been scored with

3010-519: The existing sites of the old S-25 Berkut were modified. Some known locations are: Naro-Fominsk , Olenegorsk , Skrunda , Angarsk , Nikolaeyev , and Sary Shagan . One of the Dunay radar (NATO Code : Dog House ) phased array radar systems was located at Naro-Fominsk. This system is comparable to the US's PAVE PAWS radars of the Sentinel and Safeguard ABM programs. The construction plan changed

3080-423: The fact that the missile itself is only a passive detector of a radar signal — provided by an external ("offboard") source—as it reflects off the target (in contrast to active radar homing , which uses an active radar transceiver ). Semi-active missile systems use bistatic continuous-wave radar . The NATO brevity code for a semi-active radar homing missile launch is Fox One . The basic concept of SARH

3150-535: The final attack. This can keep the target from realising it is under attack until shortly before the missile strikes. Since the missile only requires guidance during the terminal phase, each radar emitter can be used to engage more targets. Some of these weapons, like the SM-2, allow the firing platform to update the missile with mid-course updates via datalink . Some of the more effective methods used to defeat semi-active homing radar are flying techniques. These depend upon

3220-414: The front is the seeker, either a radar system, radar homer, or infra-red detector. Behind that lies the avionics which control the missile. Typically after that, in the centre of the missile, is the warhead, usually several kilograms of high explosive surrounded by metal that fragments on detonation (or in some cases, pre-fragmented metal). The rear part of the missile contains the propulsion system, usually

3290-422: The front or side aspects, as opposed to just the hotter engine nozzle(s) from rear-aspect, allowing for a true all-aspect capability. This significantly expanded potential attacking envelopes, allowing the attacker to fire at a target which was side-on or front-on to itself as opposed to just the rear. While the field-of-view was still restricted to a fairly narrow cone, the attack at least did not have to be behind

3360-488: The guidance system and manipulates the airfoils or fins at the rear of the missile that guide or steers the weapon to target. Nowadays, countries start developing hypersonic air-to-air missile using scramjet engines (such as R-37 , or AIM-260 JATM ), which not only increases efficiency for BVR battles, but it also makes survival chances of target aircraft drop to nearly zero. A number of terms frequently crop up in discussions of air-to-air missile performance. A missile

3430-426: The hot exhaust pipes of an aircraft. This meant an attacking aircraft had to maneuver to a position behind its target before it could fire an infra-red guided missile. This also limited the range of the missile as the infra-red signature soon become too small to detect with increasing distance and after launch the missile was playing "catch-up" with its target. Early infrared seekers were unusable in clouds or rain (which

3500-417: The launch aircraft has to maintain a "lock" on the target (keep illuminating the target aircraft with its own radar) until the missile makes the interception. This limits the attacking aircraft's ability to maneuver, which may be necessary should threats to the attacking aircraft appear. An advantage of SARH-guided missiles is that they are homing on the reflected radar signal, so accuracy actually increases as

3570-453: The launch aircraft vulnerable to counterattack, as well as giving the target's electronic warning systems time to detect the attack and engage countermeasures. Because most SARH missiles require guidance during their entire flight, older radars are limited to one target per radar emitter at a time. The maximum range of a SARH system is determined by energy density of the transmitter. Increasing transmit power can increase energy density. Reducing

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3640-399: The main type of guidance (with supplement of inertial guidance on initial stage). SARH missiles require tracking radar to acquire the target, and a more narrowly focused illuminator radar to "light up" the target in order for the missile to lock on to the radar return reflected off target. The target must remain illuminated for the entire duration of the missile's flight. This could leave

3710-482: The missile close to the target. At a predetermined point (frequently based on time since launch or arrival near the predicted target location) the missile's radar system is activated (the missile is said to "go active"), and the missile then homes in on the target. If the range from the attacking aircraft to the target is within the range of the missile's radar system, the missile can "go active" immediately upon launch. The great advantage of an active radar homing system

3780-500: The missile gets closer because the reflection comes from a "point source": the target. Against this, if there are multiple targets, each will be reflecting the same radar signal and the missile may become confused as to which target is its intended victim. The missile may well be unable to pick a specific target and fly through a formation without passing within lethal range of any specific aircraft. Newer missiles have logic circuits in their guidance systems to help prevent this problem. At

3850-408: The missile that allows it to home in on the jamming signal. An early form of radar guidance was " beam-riding " (BR). In this method, the attacking aircraft directs a narrow beam of radar energy at the target. The air-to-air missile was launched into the beam, where sensors on the aft of the missile controlled the missile, keeping it within the beam. So long as the beam was kept on the target aircraft,

3920-403: The missile will lock-on to it for the kill. Electro-optical seekers can be programmed to target vital area of an aircraft, such as the cockpit. Since it does not depend on the target aircraft's heat signature, it can be used against low-heat targets such as UAVs and cruise missiles . However, clouds can get in the way of electro-optical sensors. Evolving missile guidance designs are converting

3990-405: The missile would ride the beam until making the interception. While conceptually simple, the move is hard because of the challenge of simultaneously keeping the beam solidly on the target (which could not be relied upon to cooperate by flying straight and level), continuing to fly one's own aircraft, and monitoring enemy countermeasures. An added complication was that the beam will spread out into

4060-579: The noise bandwidth of the transmitter can also increase energy density. Spectral density matched to the receive radar detection bandwidth is the limiting factor for maximum range. Recent-generation SARH weapons have superior electronic counter-countermeasure ( ECCM ) capability, but the system still has fundamental limitations. Some newer missiles, such as the SM-2 , incorporate terminal semi-active radar homing (TSARH). TSARH missiles use inertial guidance for most of their flight, only activating their SARH system for

4130-414: The pilot knowing that a missile has been launched. The global positioning system allows a missile to reach the predicted intercept with no datalink, greatly increasing lethality by postponing illumination for most of the missile flight. The pilot is unaware that a launch has occurred, so flying techniques become almost irrelevant. One difficulty is testing, because this feature creates public safety risks if

4200-476: The possibility of leading a missile within its FOV for an increased probability of kill against a maneuvering target. In some cases, the improved sensitivity to heat signatures allows for a very limited side and even all-aspect tracking, as is the case with the Red Top missile . In conjunction with improved control surfaces and propulsion motors over the first generation of dogfight missiles, the technological advances of

4270-550: The projectile of the unguided 21 cm Nebelwerfer 42 infantry barrage rocket system into the air-launched BR 21 anti-aircraft rocket in 1943; leading to the deployment of the R4M unguided rocket and the development of various guided missile prototypes such as the Ruhrstahl X-4 . The US Navy and US Air Force began equipping guided missiles in 1956, deploying the USAF's AIM-4 Falcon and

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4340-402: The same time, jamming the missile lock-on is easier because the launching aircraft is further from the target than the missile, so the radar signal has to travel further and is greatly attenuated over the distance. This means that the missile may be jammed or "spoofed" by countermeasures whose signals grow stronger as the missile gets closer. One counter to this is a "home on jam" capability in

4410-467: The second-generation short-range missiles allowed them to be used not just on non-maneuvering bombers, but also actively maneuvering fighters. Examples include advanced derivatives of the K-13 (missile) and AIM-9 such as K-13M ( R-13M , Object 380) or AIM-9D / G / H . This generation introduced much more sensitive seekers that are capable of locking onto the warm heat irradiated by the skins of aircraft from

4480-409: The size of the radar antenna is limited by the small diameter of missiles, limiting its range which typically means such missiles are launched at a predicted future location of the target, often relying on separate guidance systems such as Global Positioning System , inertial guidance , or a mid-course update from either the launching aircraft or other system that can communicate with the missile to get

4550-454: The sort of accuracy needed for guidance. Instead the larger radar dish on the ground or launch aircraft will provide the needed signal and tracking logic, and the missile simply has to listen to the signal reflected from the target and point itself in the right direction. Additionally, the missile will listen rearward to the launch platform's transmitted signal as a reference, enabling it to avoid some kinds of radar jamming distractions offered by

4620-410: The target increases the probability of a hit, the launching aircraft usually has to be closer to the target in such a tail-chase engagement . An aircraft can defend against infra-red missiles by dropping flares that are hotter than the aircraft, so the missile homes in on the brighter, hotter target. In turn, IR missiles may employ filters to enable it to ignore targets whose temperature is not within

4690-440: The target on a collision course. Although the missile may use radar or infra-red guidance to home on the target, the launching aircraft may detect and track the target before launch by other means. Infra-red guided missiles can be "slaved" to an attack radar in order to find the target and radar-guided missiles can be launched at targets detected visually or via an infra-red search and track (IRST) system, although they may require

4760-446: The target. Also typical of the third generation of short-range missiles are further improved agility over the previous generation as well as their ability to radar-slave; which is acquiring tracking data from the launching aircraft's radar or IRST systems, allowing attackers to launch missiles without ever pointing the nose of the aircraft at an enemy prior to leading the missile. Examples of this generation of dogfight missiles include

4830-519: The target. The SARH system determines the closing velocity using the flight path geometry shown in Figure 1. The closing velocity is used to set the frequency location for the CW receive signal shown at the bottom of the diagram (spectrum). Antenna offset angle of the missile antenna is set after the target is acquired by the missile seeker using the spectrum location set using closing speed. The missile seeker antenna

4900-538: Was in the Dunay-3U radar systems enhanced with a dedicated sector search functionality. Along with other upgrades, actual air tests were performed with different configurations between 1976 and 1977. Phase 3 of the A-35M went on-line in 1978. Semi-active radar guidance Semi-active radar homing ( SARH ) is a common type of missile guidance system, perhaps the most common type for longer-range air-to-air and surface-to-air missile systems. The name refers to

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