Fact-checked by Grok 2 weeks ago

Active radar homing

Active radar homing (ARH) is a missile guidance method in which the missile incorporates an onboard , consisting of both a and , to independently detect, track, and intercept a by emitting signals and analyzing the reflected echoes. This autonomous terminal guidance phase distinguishes ARH from , which relies on continuous illumination from an external source, such as the launching platform's . The principles of ARH are based on monostatic radar geometry, where the missile's radar transmits pulses toward the and receives the backscattered signals along the same path. These signals are processed by an onboard computer to extract parameters like , (via Doppler shift), and angular position, which are used to calculate an optimal intercept trajectory and issue steering commands to the missile's control surfaces or thrusters. Midcourse guidance often combines inertial navigation with two-way data links from the launch to extend before activating the seeker's active mode. ARH offers significant advantages, including "" operation that permits the launching aircraft or platform to maneuver freely or engage additional threats without maintaining a continuous lock, thereby reducing to enemy defenses. It also provides all-weather, day-night capability independent of external support, enhancing operational flexibility in beyond-visual-range engagements. However, the compact size of missile-borne s limits transmitted and antenna , resulting in shorter acquisition and tracking ranges compared to larger - or platform-based systems, and increases to . The technology originated during with the U.S. Navy's , the world's first operational guided weapon employing active radar homing for anti-ship strikes, initially developed for use against submarines but employed against surface vessels in combat. Postwar advancements led to its widespread adoption in , such as the , which combined semi-active and active radar homing for long-range intercepts from carrier-based fighters starting in 1974. Contemporary examples include the , a beyond-visual-range that transitions to active radar homing in the terminal phase after inertial and data-linked midcourse guidance, with later variants achieving ranges over 100 kilometers at Mach 4 speeds. Similarly, the Russian (: AA-12 Adder) utilizes an active radar seeker for autonomous targeting at ranges up to 100 kilometers. ARH is also employed in surface-to-air and anti-ship missiles, underscoring its role in modern precision-guided munitions.

Fundamentals

Definition

Active radar homing (ARH) is a method in which the incorporates its own —comprising a , , and associated —to independently detect, track, and intercept a by analyzing radar echoes reflected from the . This onboard system enables the to operate without continuous external illumination or updates once the is acquired, making it suitable for "" applications in air-to-air and surface-to-air . The basic principle of active radar homing involves the missile's emitting pulses or continuous-wave signals toward the ; these signals reflect off the target's surface and return to the missile's , where they are processed to extract such as , , and . The guidance typically analyze the Doppler frequency shift in the returned signals to estimate the closing between the missile and , or use time-of-flight measurements for data, which are then fed into algorithms like to compute and execute trajectory corrections via control surfaces or . This closed-loop process allows the to autonomously adjust its flight path in , even against maneuvering . A key distinguishing feature of active radar homing is its autonomy during the terminal guidance phase, where the missile relies solely on its internal sensors and processors after initial target designation, unlike systems that require ongoing support from the launch . The effectiveness of this homing is fundamentally governed by the radar range equation, which quantifies the received power P_R from the target's echo: P_R = \frac{P_t G_t G_r \lambda^2 \sigma}{(4\pi)^3 R^4} Here, P_t is the transmitted power, G_t and G_r are the transmit and receive antenna gains (often equal in monostatic setups), \lambda is the radar wavelength, \sigma is the target's radar cross-section, and R is the range to the target; this equation illustrates the inverse fourth-power dependence on range, highlighting the challenges of maintaining sufficient signal strength at longer distances.

Historical Development

The origins of active radar homing trace back to , when the U.S. Navy developed the , the first operational guided weapon to employ ARH for anti-ship targeting against . Following , the initiated early experiments in radar-guided missiles, with the representing a key precursor in 1947. Developed by , the was the first U.S. to incorporate for , using a nose-mounted receiver to track targets illuminated by the launch platform's , though it primarily relied on radio command for midcourse updates. These efforts built on wartime advancements, laying groundwork for radar-guided missile systems in general, despite the Firebird's limited production and eventual cancellation due to the emergence of supersonic technology. The 1950s marked significant milestones in radar-homing missile testing, including the Sparrow program's first powered flights in late 1950, which demonstrated semi-active radar capabilities against drone targets. By mid-decade, the U.S. Navy pursued true active radar homing with the AAM-N-10 Eagle, developed around 1958 as the first such missile, featuring midcourse command guidance and an onboard active seeker adapted from the Bomarc missile's AN/DPN-53 radar. Although the Eagle program was canceled in favor of other designs, it influenced subsequent active homing efforts, while the Raytheon Sparrow series evolved from beam-riding (Sparrow I) to semi-active radar homing (Sparrow III, entering service in 1958), setting the stage for hybrid transitions. In the and , U.S. programs shifted toward integrating active capabilities to overcome semi-active limitations, particularly after experiences where pilots had to maintain radar lock on targets, restricting maneuverability and exposing them to threats. This drove the evolution of the lineage, with variants like the AIM-7E incorporating improved seekers, though full active homing awaited later generations; the emphasis on tactics emerged as a direct response to these operational constraints. The 1980s and 1990s saw breakthroughs in deployable active radar homing systems, exemplified by the , which achieved initial operational capability with the U.S. Air Force in September 1991 as the first widely fielded . Paralleling this, the introduced the (NATO: AA-12 Adder) around 1994, featuring an active radar seeker for beyond-visual-range engagements and entering service with Russian forces to counter Western advancements. From the 2000s onward, active radar homing integrated advanced technologies like (AESA) seekers for enhanced resistance to and low-observable targets. The Meteor, a ramjet-powered with active guidance, achieved initial operational capability with the Air Force's Gripen fighters in 2016, extending engagement ranges through sustained . Upgrades to existing systems, such as the AIM-120D introduced in the , added two-way data links for network-enabled targeting, allowing mid-flight updates from offboard sensors to improve accuracy against stealthy threats. These developments have solidified active radar homing's role in modern air superiority, enabling independent terminal guidance and reducing pilot workload in contested environments.

Comparisons with Other Guidance Methods

Semi-Active Radar Homing

() is a guidance method in which the launching platform, such as an or ground-based system, continuously illuminates the target with energy throughout the 's flight. The itself does not transmit signals but instead contains a that detects and homes in on the reflected waves from the target. This approach relies on the illuminator's to provide the primary energy source, making the a passive seeker in terms of . In terms of , the employs techniques such as monopulse or conical to accurately the target's reflected signals and adjust its accordingly. Monopulse systems divide the beam into multiple lobes to determine angular errors precisely, while conical involves a rotating beam pattern that the decodes for guidance commands. A key operational requirement is that the launching platform must maintain a continuous line-of-sight to the target until impact, as any interruption in illumination causes the to lose guidance. This line-of-sight dependency limits the engagement geometry, typically restricting effective use to forward or near-forward quadrants relative to the illuminator. Historically, was the predominant radar guidance technology for missiles from the 1950s through the 1980s, exemplified by the , which entered service with the U.S. Navy in 1958 and relied on ship or illumination for terminal homing. It remained in widespread use for decades, with like the AIM-7M improving range and accuracy but still bound by illuminator constraints. Ground-based systems, such as the Soviet S-75 (SA-2 Guideline) introduced in 1957, also utilized SARH, achieving notable success in engagements like the downing of U-2 spy planes, though later iterations persist in modernized forms for legacy defenses. The primary limitations of SARH that spurred the development of include the need for the launching platform to sustain lock, which exposes it to enemy detection and counterfire, and imposes restrictions on the shooter's maneuverability during the engagement. For instance, pilots had to maintain a steady toward the , limiting evasive actions and increasing vulnerability in dogfights. These drawbacks highlighted the need for self-contained , leading to active systems. SARH designs significantly informed early (ARH) prototypes through shared seeker technologies, such as monopulse receivers adapted for onboard transmission in missiles like the , which evolved from lineage in the 1980s.

Passive Homing Systems

Passive homing systems guide missiles by detecting and tracking natural or enemy-generated emissions without the missile emitting its own signals, relying instead on sensors to receive energy from the target such as radar waves or heat signatures. This approach contrasts with active radar homing, where the missile transmits radar pulses to illuminate and detect the target, making passive methods inherently stealthier as they produce no detectable emissions during flight. Key types include homing, which targets enemy radar emissions using anti-radiation missiles like the , a supersonic air-to-surface weapon designed to seek and destroy radar-equipped air defense systems. Another prominent type is () homing, which detects thermal signatures from targets such as aircraft engines, exemplified by the , a heat-seeking air-to-air missile that entered U.S. service in 1956. In homing mechanics, the missile employs a broadband receiver to detect the direction and strength of radar emissions from the target, allowing it to home in without requiring external illumination or its own transmissions, thus enabling a covert approach until impact. Compared to active radar homing, passive systems offer lower detectability since the missile remains "quiet" and does not reveal its position through emissions, reducing the risk of counter-detection by enemy defenses. They also provide partial immunity to certain radar jamming techniques that target active seekers, as passive homing depends on the target's own signals rather than missile-generated ones. Historically, early IR homing appeared in the 1950s with the , the first operational U.S. guided developed from 1946 onward, while anti-radiation missiles like the saw combat debut during the in 1965 to suppress North Vietnamese radar sites. However, passive homing is limited by its dependence on the target actively emitting signals; if the source ceases transmission, the may lose guidance and continue on a ballistic path. IR homing faces additional constraints from atmospheric absorption of heat signatures, particularly in humid or cloudy conditions, which restricts effective ranges to shorter distances compared to radar-based systems.

Operational Principles

System Components

Active radar homing systems integrate a compact radar transceiver within the to enable autonomous and tracking in the terminal phase. The consists of a miniaturized and , typically operating in the X-band (8-12 GHz) for high resolution, using solid-state components for pulse-Doppler waveforms that measure range and velocity. Antennas are often slotted arrays, which provide mechanical scanning via mechanisms for , or active ally scanned arrays (AESAs) that employ scanning through phase shifters in transmit/receive (T/R) modules for rapid, jitter-free beam agility. Signal processing is handled by an onboard digital computer that implements algorithms for target discrimination and clutter rejection. Key techniques include (CFAR) processing, which adaptively sets detection thresholds based on local noise statistics to maintain a consistent probability amid varying . Additional algorithms support multiple target tracking by correlating returns across pulses, using Doppler filtering to isolate moving targets from ground or sea clutter. These processes rely on high-speed processors, such as field-programmable gate arrays (FPGAs), to meet demands in constrained computational environments. Power and cooling systems are critical for sustaining emissions in a compact . Primary power sources include thermal batteries, activated upon launch to provide high-energy density for short-duration operation, or generators in larger missiles that convert airflow into electrical during flight. Thermal management employs passive heat sinks and conductive materials to dissipate heat from high-power transmitters, preventing performance degradation in the seeker's . Integration occurs within the seeker head assembly, where the and are housed behind a made of radar-transparent materials like glass-fiber reinforced plastic (GFRP) to minimize signal and errors. The seeker interfaces with the missile's () via data links, allowing midcourse updates to refine the search sector before active homing activation. This setup ensures seamless transition from inertial guidance to radar-based terminal control. Modern enhancements focus on ()-based amplifiers, which offer higher power efficiency and heat tolerance compared to (GaAs) predecessors, enabling compact transmitters with reduced cooling needs. Digital in AESA seekers further improves by forming multiple simultaneous beams for enhanced tracking and (ECCM) resilience. These advancements support longer detection ranges and better performance in contested environments.

Guidance Phases

Active radar homing missiles typically operate through a sequence of distinct guidance phases that transition the weapon from platform-dependent to fully autonomous , enabling capability once the terminal phase begins. These phases—launch, midcourse, and terminal—coordinate inertial systems, data links, and the onboard seeker to progressively refine the toward the . During the launch phase, the missile undergoes initial boost propulsion to achieve flight speed, relying on inertial guidance or coarse targeting cues provided by the launching platform's for an initial flight path. The seeker remains caged or in standby mode to conserve power and avoid interference, with flight controls often locked in a neutral position until aerodynamic stability is established. This short-duration phase positions the missile for subsequent without active emissions. In the midcourse phase, the employs inertial navigation to follow a precomputed ballistic or commanded trajectory, closing the range to the target area while receiving occasional updates via a two-way from the launch platform. These updates, such as refined target position or midcourse corrections, are processed by the 's onboard computer to adjust the flight , ensuring optimal for later seeker acquisition. The seeker stays inactive during this extended phase, which can involve external sensor tracking of the target to minimize onboard resource use. The terminal phase marks the shift to autonomy, with the radar seeker activating at a predetermined range, typically 10-20 km, to illuminate and lock onto the target independently. Once locked, the missile uses proportional navigation to guide itself to intercept, commanding lateral acceleration according to the law a = N \cdot V_c \cdot \dot{\lambda}, where a is the missile's acceleration perpendicular to the line of sight (LOS), N is the navigation constant (typically 3-5 for optimal performance against non-maneuvering targets), V_c is the closing velocity, and \dot{\lambda} (or d\lambda/dt) is the LOS angular rate. This law ensures the missile rotates its velocity vector at a rate proportional to the target's apparent motion, minimizing miss distance by nulling the LOS rate at impact. The handover process facilitates a seamless transition from external midcourse cues to internal guidance, where the seeker uncages and acquires the based on predicted , correcting any perpendicular displacement errors. In scenarios, such as low-altitude engagements, the system handles clutter and ground returns through seeker stabilization and designs that reduce signal distortion, enabling reliable lock-on despite environmental challenges. The endgame within the terminal phase involves high-G maneuvers driven by real-time radar data, utilizing aerodynamic surfaces or to execute tight turns and counter target evasion. This culminates in precise impact, with the guidance law providing rapid response to maintain convergence.

Advantages and Challenges

Advantages

Active radar homing provides a fire-and-forget capability, allowing the to guide itself autonomously after launch without requiring continuous illumination or support from the launching platform. This enables the , such as an , to maneuver evasively, disengage early, or engage additional threats immediately following launch. In the terminal phase, the missile's proximity to the target significantly improves guidance accuracy, as the seeker operates at much shorter than the launch platform would. The received signal strength increases dramatically due to the fourth-power dependence on range in the radar equation, enhancing and resolution for precise hit-to-kill intercepts. Active radar homing offers resistance to jamming directed at the launch platform, since the target's electronic countermeasures cannot easily disrupt the distant shooter while the missile's onboard seeker—due to its small size and low-power emissions—is harder to detect and selectively jam. The system supports all-weather and day/night operations, as radar signals penetrate clouds, rain, fog, and smoke without degradation from visibility limitations that affect infrared seekers. It facilitates multiple target engagements, permitting the launching to fire several in rapid succession against independent targets without needing sustained radar support for each. This guidance method enhances tactical flexibility by enabling beyond-visual-range engagements with minimized risk to the launch , as the autonomous homing reduces exposure during the flight.

Disadvantages and Countermeasures

Active radar homing systems face significant technical limitations primarily due to the constraints of within airframes. The small size of the onboard restricts the (ERP), resulting in a detection range typically limited to 20-50 km for the seeker, compared to over 100 km for larger platform-based s. Additionally, the high power requirements of the strain battery resources, curtailing operational time and necessitating careful management of seeker activation to preserve energy for the terminal phase. The complexity of integrating compact radar components also contributes to elevated costs and early reliability challenges. Active radar seekers can account for a substantial portion of the missile's expense, with units like the AIM-120D costing approximately $1.09 million each (FY 2019), driven by advanced and efforts. In initial developments of compact active seekers, such as the , miniaturization contributed to early reliability challenges with guidance and control systems, requiring extensive testing to achieve dependable performance. However, recent advancements like (AESA) seekers and low-probability-of-intercept (LPI) modes in missiles such as the AIM-120D-3 (introduced 2023) improve resistance to detection and jamming. A key vulnerability of active radar homing is the detectability of its emissions, which broadcast the missile's presence and trajectory to defensive systems. Unlike passive homing methods, the onboard transmitter's signals can be intercepted by the target's radar warning receivers, enabling evasive actions such as beam maneuvers or deployment of countermeasures before impact. Effective countermeasures against active radar homing include electronic jamming, which disrupts seeker operation through noise or techniques. Noise jamming overwhelms the with random signals across the missile's frequency band, while methods, such as range or Doppler spoofing, create false to mislead guidance. deployment generates reflective clouds that produce multiple false echoes, saturating the seeker's tracking capability and diverting it from the true . Platform-based defenses further mitigate threats from active radar missiles. Digital radio frequency memory (DRFM) jammers capture, modify, and retransmit the seeker's pulses to spoof its , creating illusory targets or velocity shifts that break lock. —flying perpendicular to the missile's radar beam—minimizes the target's Doppler shift relative to the seeker, exploiting pulse-Doppler processing limitations to reduce detection probability. Stealth designs that reduce radar cross-section () pose modern challenges to active radar homing effectiveness. Low-RCS aircraft like the F-35, with an estimated frontal RCS of 0.001-0.01 , significantly lower the probability of seeker acquisition and sustained tracking, particularly in beyond-visual-range engagements. Combined threats may also prompt the use of flares or launchers, though these are more effective against seekers, underscoring the need for integrated defensive suites.

Applications

Air-to-Air Missiles

Active radar homing plays a pivotal role in beyond-visual-range (BVR) engagements for , allowing missiles to autonomously track and intercept targets after launch without requiring continuous illumination from the launching platform. This capability enables pilots to execute salvo launches against multiple threats simultaneously, preserving the shooter's tactical position and maneuverability in contested airspace. For instance, the employs inertial mid-course guidance followed by active radar terminal homing, facilitating rapid, independent in all-weather conditions. Performance in air-to-air scenarios demands high-speed propulsion and agile control systems to counter evasive maneuvers by modern fighters. Typical active radar-guided missiles achieve velocities of 3 to 4, enabling quick closure rates over extended distances while maintaining stability during high-g turns. The seeker's active radar typically activates 10-30 km from the target to optimize energy management and minimize detection risk, integrating seamlessly with the launch aircraft's radar for initial cueing—such as the on the F-14 Tomcat, which supported simultaneous guidance for up to six missiles with terminal active homing. Tactically, these missiles support multi-shot salvos in networked environments, where data links from airborne early warning systems or cooperative provide mid-course updates, enhancing saturation attacks against enemy formations. This autonomy indirectly aids by allowing launch platforms to disengage immediately, reducing exposure to surface threats during BVR operations. The evolution of active radar homing in air-to-air missiles has progressed from early implementations like the , with effective ranges of 50-100 km, to advanced designs such as the MBDA Meteor, which leverages propulsion for sustained velocity and a no-escape zone of over 60 km against maneuvering targets. Key challenges include mitigating high clutter returns from ground or sea environments, particularly in low-altitude engagements, necessitating advanced for target discrimination. capability is essential to avoid terrain masking, with modern employing Doppler filtering and adaptive waveforms to isolate targets amid such interference.

Surface-to-Air and Anti-Ship Missiles

Active radar homing plays a critical role in (SAM) systems, enabling the interception of and cruise missiles launched from ground-based sites. These missiles typically employ active radar during the terminal phase to autonomously track and engage targets after midcourse guidance via inertial or data links from ground radars. For instance, the Russian S-400 system's 40N6 missile utilizes active radar homing to achieve intercepts at extended ranges, providing high hit probability against aerodynamic targets including low-flying cruise missiles. Similarly, the U.S. PAC-3 interceptor incorporates an active Ka-band radar seeker for precise terminal guidance, enhancing its effectiveness in layered air defense against maneuvering threats. In anti-ship applications, active radar homing allows missiles to home in on vessels characterized by large radar cross-sections (RCS), often integrating with shipboard radars for over-the-horizon targeting. The U.S. Navy's RGM-84 Harpoon missile employs active radar terminal homing to detect and strike surface ships while flying at sea-skimming altitudes, minimizing exposure to defenses. Likewise, the Russian 3M-54 Kalibr anti-ship variant activates its active radar seeker in the final phase to engage naval targets, combining inertial midcourse guidance with autonomous terminal acquisition for improved accuracy against moving ships. Adaptations for ground and sea launch platforms include extended midcourse phases supported by booster rockets, which propel SAMs to high altitudes for broader engagement envelopes, as seen in the S-400's multi-stage design. Active radar seekers in anti-ship missiles are engineered to resist sea clutter interference, using to discriminate ship returns from ocean waves during low-altitude flights. Vertical launch compatibility is a key feature in modern systems, allowing rapid, all-aspect firing from canisters or silos without rail mechanisms; for example, the Evolved SeaSparrow Missile (ESSM) Block 2 uses active radar homing and fits into standard vertical launch systems for shipboard deployment. Tactically, active radar homing supports area defense roles in SAM networks, such as the PAC-3's integration into integrated air defense systems to protect fixed sites from aerial incursions. Certain advanced SAMs exhibit anti-satellite potential during exo-atmospheric phases, where active radar guidance could theoretically extend to intercepting low-earth objects, though primary designs focus on atmospheric threats. Performance metrics highlight ranges up to 400 km for sophisticated SAMs like the 40N6, enabling strategic depth in defense. Anti-ship missiles prioritize low-altitude sea-skimming trajectories, with the maintaining altitudes as low as 15-60 meters to evade radar detection en route to targets.

Inventory by Country

Americas

The leads in active radar homing missile technology within the , with the AIM-120 Advanced Medium-Range (AMRAAM) serving as a primary example since achieving initial operational capability in September 1991. This employs active radar homing in its phase, with effective ranges spanning approximately 50 km for early variants like the AIM-120A to over 160 km for the AIM-120D, enabling all-weather engagements against agile targets. The AIM-120D variant incorporates seeker upgrades for enhanced electronic counter-countermeasure resistance and navigation accuracy, supporting integration on such as the F-15, F-16, and F-22. Over 20,000 AMRAAM units have been produced for U.S. and allied forces, reflecting its widespread adoption, though exports are strictly controlled under the (ITAR) to prevent proliferation of sensitive technology. Earlier U.S. efforts laid the groundwork for active radar systems through the , which transitioned from beam-riding guidance in initial models to in variants like the AIM-7E and AIM-7M, influencing the shift to fully autonomous active homing in successors. In the naval domain, the RIM-174 Standard Missile 6 (SM-6) provides multi-role active radar homing for surface-to-air, anti-ship, and defense applications, with its dual-mode seeker enabling independent target acquisition at extended ranges beyond 370 km. Canada lacks indigenous active radar homing missiles but has integrated the AIM-120 AMRAAM into the National Advanced Surface-to-Air Missile System (NASAMS) through collaborative procurement and production efforts with the United States and Norway, enhancing ground-based air defense capabilities.

Europe

France has pioneered several active radar homing systems, with the MBDA MICA missile representing a key advancement in dual-mode technology. Introduced in 1996, the MICA features both infrared and active radar homing (RF) variants, enabling all-weather, fire-and-forget operations in beyond-visual-range (BVR) and short-range engagements, with a typical range of 60-80 km. This versatility allows integration on platforms like the Rafale and Mirage 2000, supporting multi-role air dominance missions. Complementing the MICA, the Aster 30 surface-to-air missile employs active radar homing in its terminal phase for high-agility intercepts, achieving ranges exceeding 120 km against aircraft, cruise missiles, and short-range ballistic threats. Developed jointly by France and Italy, the Aster 30 emphasizes 360-degree coverage and rapid reaction times, enhancing layered air defense capabilities. Multinational collaboration under , involving , the , , , , and , has produced the beyond-visual-range , entering service in 2016. Powered by a engine, the uses active radar homing to maintain high speed and maneuverability throughout its flight, delivering a range over 200 km and creating an expansive no-escape zone—several times larger than conventional solid-rocket missiles—due to sustained propulsion that enables late-course target adjustments. This design prioritizes endgame lethality in contested airspace, with integration on platforms such as the , Rafale, and Gripen. has also pursued upgrades to the short-range missile, enhancing its performance for air-to-air roles, though it remains primarily infrared-guided with potential adaptations for broader European systems. Sweden's contributions include the RBS-15 , a system with terminal active homing for precision strikes against naval targets. The Mk3 variant offers a exceeding 200 km, featuring sea-skimming trajectories, all-weather , and land-attack capabilities through inertial augmented by GPS and a J-band seeker. Deployable from ships, , or coastal launchers, the RBS-15 underscores Sweden's focus on flexible, autonomous maritime defense. Additionally, Diehl Defence's , traditionally an infrared-homing , is exploring active homing variants in testing to expand its multi-role potential, including dual-mode seekers for improved target discrimination in complex environments. Among other European developments, the IRIS-T SL stands out as a ground-launched surface-to-air missile system with active radar homing integration in its advanced configurations, such as the SLX variant, which combines radar and infrared guidance for medium-range intercepts up to 40 km. These systems highlight Europe's emphasis on interoperability within NATO frameworks, where missiles like the Meteor and MICA facilitate seamless integration across allied platforms and enhance collective air and maritime superiority.

Asia

In Asia, active radar homing (ARH) technology has seen significant advancement, particularly among major powers like , , , and , driven by regional security needs and efforts toward self-reliance in missile systems. These nations have developed ARH missiles for air-to-air and surface-to-air applications, often building on indigenous innovations while incorporating influences from collaborations and exports. Russia's extensive ARH missile portfolio has notably shaped regional inventories through exports, especially to India, while and emphasize rapid to reduce foreign dependencies. China's (export designation SD-10) represents an early indigenous ARH beyond-visual-range , introduced in 2005 with a range of 70-100 km, featuring an seeker for . The missile employs inertial navigation with mid-course updates, transitioning to autonomous ARH in the terminal phase to engage targets independently. Building on this, the , a more advanced long-range ARH , exceeds 200 km in range and incorporates an (AESA) seeker for enhanced detection and resistance to jamming. In surface-to-air applications, the system's later variants, such as the HQ-9B, utilize ARH for , combining mid-course with active terminal acquisition to improve hit probability against maneuvering aircraft and cruise missiles at ranges up to 200 km. Russia, as a Eurasian power, maintains a leading role in ARH missile development, with systems influencing Asian inventories through exports. The (NATO: AA-12 Adder), operational since 1994, is a medium-range ARH with an 80-110 km range, using inertial guidance, data-link updates, and an active seeker that activates around 20 km from the target for capability. For extended engagements, the R-37 offers a long-range ARH option exceeding 300 km, employing a dual-mode seeker with semi-active and active homing to target high-value assets like airborne early warning at hypersonic speeds. Russia's surface-to-air systems further exemplify ARH integration: the S-400 employs the 40N6 for ultra-long-range intercepts up to 400 km, relying on active guidance to engage low-maneuverability targets such as AWACS platforms; similarly, the S-500's 77N6 features an onboard active phased-array seeker for hypersonic threat interception. India has pursued aggressive indigenization of ARH technology, partly inspired by Russian exports like the integrated on Su-30MKI fighters, to develop homegrown alternatives. The Mk1, inducted in 2020, is an indigenous beyond-visual-range ARH with an 80-110 km range, utilizing inertial guidance, mid-course data-link corrections, and a terminal active seeker effective up to 25 km for precise intercepts. Complementing this, the surface-to-air missile incorporates a Ku-band active seeker for terminal homing, extending engagement range to 70-80 km while enhancing autonomy against low-altitude threats like drones and cruise missiles. These developments reflect India's shift toward 90% indigenous content in missile systems, reducing reliance on imports. Japan's ARH missiles focus on defensive air superiority and strike capabilities. The (Type 99), a medium-range ARH with approximately 100 km range, uses an active seeker for beyond-visual-range engagements, allowing independent targeting of multiple threats from F-15J and F-2 aircraft. In anti-ship roles, the ASM-2 (Type 93) employs inertial navigation with terminal active radar homing to strike surface vessels at ranges up to 180 km, improving accuracy in cluttered environments.

Middle East and Africa

In the Middle East, Israel has been a pioneer in developing compact active radar homing (ARH) seekers for air-to-air and surface-to-air missiles, enabling integration into smaller airframes while maintaining high performance in contested environments. The Rafael Advanced Defense Systems Derby missile, introduced in 1998, features an advanced RF seeker for beyond-visual-range engagements with a reported range exceeding 50 km, and its extended-range variant (I-Derby ER) achieves up to 100 km through dual-pulse propulsion and fire-and-forget capability. This design emphasizes miniaturization of the radar seeker to fit diverse platforms, including fighter jets and unmanned systems, contributing to Israel's export success, such as the adaptation for India's Astra missile program. Complementing this, the Barak-8 surface-to-air missile, jointly developed with India since 2006, employs a terminal-phase active radar seeker for 360-degree coverage and intercepts at ranges up to 70 km, with thrust vector control enhancing maneuverability against agile threats. Iran has pursued reverse-engineering and indigenous adaptations of ARH technology amid sanctions, focusing on long-range air-to-air capabilities for its aging fleet. The , a domestically produced derivative of the U.S. introduced around 2004, incorporates an active radar homing guidance system for independent terminal acquisition, achieving a range of approximately 150-160 km and speeds when launched from F-14 aircraft. For surface-to-air defense, the system, unveiled in 2019 and entering serial production by 2025, uses missiles with guidance, though Iranian sources claim enhancements toward full active capability for intercepts up to 300 km; it integrates with domestic radars to counter aircraft and ballistic missiles. In , South Africa's has emphasized ARH upgrades to bolster short- and medium-range defenses, particularly for naval and air platforms. The , a beyond-visual-range developed in the 1990s and tested on Cheetah fighters, relies on an active radar homing seeker for all-aspect engagements at ranges up to 60 km, filling a gap in radar-guided munitions during embargo-era innovations. The Umkhonto , operational since 2001 primarily with guidance for ship-based intercepts up to 20 km, is undergoing upgrades to an ARH variant (Umkhonto-R) announced in 2025, replacing the IR seeker with radar for all-weather performance and integration with systems like the . Other Middle Eastern nations, such as Turkey, have advanced indigenous ARH programs to reduce import dependence. Turkey's TÜBİTAK SAGE Gökdoğan missile, a beyond-visual-range air-to-air system tested successfully in 2025 from F-16 aircraft, features an active radar seeker with mid-course data-link updates for ranges over 100 km, marking a shift toward self-reliance in BVR combat. For anti-ship roles, the SOM-J cruise missile variant, fired in live tests in October 2025, employs inertial/GPS guidance with a terminal active radar seeker for sea-skimming precision strikes at standoff distances exceeding 250 km. Regional inventories heavily rely on imports, exemplified by Saudi Arabia's acquisition of over 1,000 U.S. AIM-120C-8 AMRAAM missiles approved in 2025, providing ARH capability for F-15 platforms at ranges up to 120 km to counter aerial threats in the Persian Gulf.

Other Regions

Australia relies heavily on imported active radar homing missiles through its alliance with the United States, lacking indigenous production capabilities for such systems. The Royal Australian Air Force integrates the , which employs active radar homing for beyond-visual-range engagements, with recent procurements including up to 400 AIM-120D-3 and AIM-120C-8 variants to enhance air defense and strike capabilities across the Australian Defence Force. Additionally, the Australian military has adopted the , featuring multi-mode guidance that incorporates passive and active radar elements for terminal homing against maritime targets, with operational testing completed in 2025. In Taiwan, efforts toward self-reliance have led to the development of domestic active radar homing missiles, exemplified by the TC-1, also known as the Sky Sword II, a beyond-visual-range air-to-air missile with an seeker for and a reported range of approximately 65 kilometers. The Hsiung Feng series further bolsters anti-ship defenses, with the Hsiung Feng II utilizing dual active radar and infrared homing in its terminal phase, while the supersonic Hsiung Feng III employs inertial navigation augmented by active radar homing to achieve ranges exceeding 100 kilometers against naval threats. South Korea has pursued indigenous advancements in active radar homing technology amid regional tensions, with the Cheongung (also designated M-SAM or KM-SAM) surface-to-air missile system featuring upgraded variants that incorporate for hit-to-kill intercepts of and ballistic missiles at ranges up to 40 kilometers and altitudes of 15 kilometers. Recent enhancements to the Cheongung Block-II emphasize for improved response against short- and medium-range threats, achieving speeds of Mach 4.5. Across these regions, particularly in Oceania and East Asia, active radar homing missile inventories reflect strong dependence on U.S. alliances for core systems like the , while Taiwan and South Korea advance local production to reduce vulnerabilities and enhance strategic autonomy.

References

  1. [1]
    Chapter 15 Guidance and Control - Military Analysis Network
    A combination of command guidance and semi-active homing guidance is a type of hybrid guidance. It achieves many advantages of both systems. It attains long ...
  2. [2]
    AIM-120 AMRAAM Slammer
    ### Summary of Active Radar Homing for AIM-120 AMRAAM
  3. [3]
    The Birth of Guided Missiles | Proceedings - U.S. Naval Institute
    The Bat missile was the world's first guided missile with active homing radar. The officer responsible for design, development, testing, and procurement was ...
  4. [4]
    AIM-54 Phoenix Missile - GlobalSecurity.org
    Jun 12, 2017 · Semi-active and active homing radar and hydraulically operated fins direct and stabilize the missile on course to the target. Propulsion is ...
  5. [5]
    AA-12 ADDER R-77 - GlobalSecurity.org
    Feb 6, 2018 · The R-77 missile has an active radar finder and a maximim range of 90-100 kilometers (50 km more than AMRAAM) and flies at four times the speed of sound.
  6. [6]
    [PDF] Basic Principles of Homing Guidance - Johns Hopkins APL
    INTRODUCTION. The key objective of this article is to provide a broad conceptual foundation with respect to homing guidance.
  7. [7]
    ACTIVE AND SEMIACTIVE RADAR MISSILE GUIDANCE
    Probably the most extreme example of what they are capable of, is the Hughes AIM-54 Phoenix. Launched from the F-14, the weapon is targeted by the large AWG-9 ...
  8. [8]
    The Radar Equation - Radartutorial
    ### Summary of the Radar Range Equation (Monostatic Radar)
  9. [9]
    Ryan AAM-A-1 Firebird - Designation-Systems.Net
    Sep 8, 2004 · It was directed toward the target by an operator using a radio command guidance system, and used semi-active radar guidance for terminal homing.
  10. [10]
    The Development of Radar Homing Missiles - AIAA ARC
    The December 1950 flight ushered in the crucial decade in homing missile history.
  11. [11]
    Backgrounder - AIM-54 Phoenix Missile - NAVAIR - Navy.mil
    Oct 5, 2004 · Guidance System: Semi-active and active radar homing ... AIM-54 Phoenix was a product of two US missile programs – the Navy's Bendix AAM-N-10 ...
  12. [12]
    Armaments and Innovation - U.S. Naval Institute
    In 1952, a Sparrow I successfully intercepted an F6F Hellcat fighter at a range of 4,000 yards. The missile joined the fleet on F3H-2M Demon fighters beginning ...
  13. [13]
    AIM-120 AMRAAM > Air Force > Fact Sheet Display - AF.mil
    The AMRAAM program completed its conceptual phase in February 1979 when the U.S. Air Force selected two of five competing contractors, Hughes Aircraft Co. and ...
  14. [14]
    R-77 (AA-12A Adder) Russian Air-to-Air Missile - ODIN
    May 30, 2025 · The R-77 missile features an energetic radar seeker and a range of 90-100 kilometers (50 km more than AMRAAM) and flies at four times the speed of sound.Missing: service entry
  15. [15]
    Meteor - Beyond Visual Range Air-to-Air Missile (BVRAAM)
    Jul 7, 2021 · In July 2016, the Meteor missile was fully integrated into the Swedish Air Force's Gripen fighter aircraft. With the integration, Gripen became ...
  16. [16]
    Iconic AIM-120 AMRAAM missile is getting a high-tech new upgrade
    Jul 18, 2025 · Yet, it has been publicly disclosed that these missiles boast a two-way data link that allows for third-party targeting at long ranges – this ...
  17. [17]
    [PDF] Guest Editor's Introduction: Homing Missile Guidance and Control
    In active seeker guidance systems, an illuminator (transmitter) is added to the missile. Hence, an active guidance system can self-illuminate the target ...
  18. [18]
    Principles of Guided Missiles and Nuclear Weapons
    If the target emits the homing stimulus, the system used to detect the target and guide the missile to it is known as a PASSIVE HOMING guidance system. One ...
  19. [19]
    AGM-88 HARM (high-speed antiradiation missile) - Smart Weapons
    Apr 23, 2000 · The AGM-88 HARM (high-speed antiradiation missile) is a supersonic air-to-surface tactical missile designed to seek and destroy enemy radar-equipped air ...
  20. [20]
    AIM-9 Sidewinder > Air Force > Fact Sheet Display - AF.mil
    The AIM-9A, a prototype of the Sidewinder, was first fired successfully in September 1953.
  21. [21]
    Hughes AAM-A-2/F-98/GAR-1,2,3,4/AIM-4 Falcon
    Jul 24, 2008 · The Falcon was the first operational guided air-to-air missile of the US Air Force. Development started in 1946, when Hughes was awarded a contract to study a ...Missing: history | Show results with:history
  22. [22]
    AGM-45 Shrike Anti-Radar Missile - Air Force Museum
    Originally developed by the U.S. Navy from the Sparrow air-to-air missile, the anti-radar AGM-45 Shrike homed on and destroyed radar emitters.
  23. [23]
    Heat-Seeking Missile Guidance - Air Power Australia
    The atmosphere basically affects IR energy in three different ways - absorption, scattering and scintillation (for a more detailed treatment see TE Dec.1981, ...
  24. [24]
    [PDF] Guidance and Homing of Missiles and Pilotless Aircraft - DTIC
    of radar's chief advantages is its usefulness 24 hours each day. ... report describes the general principles, problems, and state of development of radar homing.
  25. [25]
    [PDF] Advances in Active Radar Seeker Technology - CORE
    Active radar seekers have gained wide applications in the terminal phase of missile guidance to provide hit-to-kill capability.
  26. [26]
  27. [27]
    How do relatively small missiles like the Patriot PAC-3 and AIM-120 ...
    Jan 21, 2020 · Instead they must use a battery instead, which severely limits the power and thus range of the radar - typically to far less than the range of ...When and how can semi-active radar homing be superior to ... - QuoraWhy are active radar homing missiles generally just as small ... - QuoraMore results from www.quora.com
  28. [28]
    Packing a punch | Raytheon - RTX
    Radars and missiles are just the beginning, as GaN technology also has the potential to replace any radio frequency application that requires high power and ...
  29. [29]
    Precision-Guided Munitions: Radar-Guided Weapons (Part 4 of 4)
    Sep 30, 2015 · Looking at disadvantages, active radar guided missiles are likely to have increased size and weight as compared to missiles employing semi- ...
  30. [30]
    [PDF] Modern Homing Missile Guidance Theory and Techniques
    Classical guidance laws, with proportional navigation (PN) being the most prominent example, had proven to be effective homing guidance strategies up through ...
  31. [31]
    None
    Below is a merged response summarizing the advantages of active radar homing in missile guidance and control systems, consolidating all information from the provided segments. To retain maximum detail, I’ve organized the data into a table in CSV format, which includes page references, quotes, and additional context from each segment. Following the table, I provide a narrative summary that integrates the key points while avoiding redundancy.
  32. [32]
    [PDF] ELECTRONIC COMBAT SYSTEMS - DTIC
    proportional to the fourth power of the distance. In a beacon system, the ... Active radar homing is contained within the missile and is a complete ...
  33. [33]
    The Silent Hunter: Ultimate Guide to the AMRAAM Missile
    Jul 1, 2025 · The AIM-120D significantly extends the missile's range to around 86 nautical miles (99 miles/160 kilometers) or potentially even beyond 100 ...
  34. [34]
    Chapter 11 COUNTERMEASURES - Military Analysis Network
    The first method encompasses most jamming and deception techniques. The second includes such techniques as chaff dispersion. The third way includes applying ...
  35. [35]
    Impact analysis of DRFM-based active jamming to radar detection ...
    The purpose of this paper is to analyse the energy of the jamming signal and use the suppression jamming method based on DRFM technology [1, 2]. In the ...
  36. [36]
    Anti-BVR tactics | Key Aero
    A couple of combat accounts in the 1991 Gulf War seem to suggest Doppler notch maneuver was effective in breaking radar lock. In the age of AESA radar and.Missing: homing | Show results with:homing
  37. [37]
    [OPINION] F-35A vs S-400 Triumf: a quick analysis on open source ...
    Sep 3, 2024 · According to independent simulation results, the RCS of the F-35 without RAM (Radar Absorbing Materials) is 0,09 m² in X-band and 0,15 m² in S- ...
  38. [38]
    AIM-120 AMRAAM - Advanced Medium Range Air-to-Air Missile
    In September 1991, IOC (Initial Operational Capability) was achieved for the AMRAAM on USAF F-15 aircraft. The F-16 followed in January 1992, and the Navy ...Missing: date | Show results with:date
  39. [39]
    Hughes AIM-120 AMRAAM - Air Force Museum
    The AMRAAM weighs 340 pounds and uses an advanced solid-fuel rocket motor to achieve a speed of Mach 4 and a range in excess of 30 miles. In long-range ...
  40. [40]
    Raytheon AIM-54C Phoenix - Estrella Warbirds Museum
    3 ft (910 mm) · 135 lb (61 kg), high explosive · Semi-active radar homing and terminal phase active radar homing · F-14 Tomcat · Approximately: $477,131.
  41. [41]
    AMRAAM Missile | Raytheon - RTX
    It is the only radar-guided, air-to-air missile cleared to fly on the F-35. The AMRAAM is truly a dual-role missile, offering operational flexibility in air-to- ...
  42. [42]
  43. [43]
    Meteor | MBDA Inc.
    With its advanced active radar seeker, Meteor engages current and future air targets, ranging from fast jets to UAVs and cruise missiles, day or night, in all ...
  44. [44]
    Meteor Beyond Visual Range Air-to-Air Missile (BVRAAM
    Produced by MBDA, Meteor is an active radar guided missile designed to provide a multi-shot capability against long-range maneuvering targets, such as fast jets ...
  45. [45]
    S-400 Triumph Air Defence Missile System - Army Technology
    Feb 3, 2020 · The 40N6 missile of the S-400 has a claimed range of 400km and uses active radar homing to intercept air targets at great distances. It can ...
  46. [46]
    The ultimate guide to the Patriot air defense system - Sandboxx
    Mar 5, 2025 · PAC-3 missiles use an active Ka-band radar seeker for terminal guidance into the target, with 180 solid-fueled attitude control motors (ACM) in ...Missing: homing | Show results with:homing
  47. [47]
    Harpoon Missile > United States Navy > Display-FactFiles
    Sep 28, 2021 · Guidance System: Sea-skimming cruise monitored by radar altimeter/ active radar terminal homing. Point of Contact Program Executive Office
  48. [48]
    3M-54 Kalibr/Club (SS-N-27) | Missile Threat - CSIS
    Jan 9, 2017 · The 3M-54 Kalibr/Club (SS-N-27) is a Russian short-range, ship- and submarine-launched anti-ship cruise missile, with a range of 220 km (3M54) ...
  49. [49]
    S-400 SA-21 Triumf Missiles - GlobalSecurity.org
    Oct 4, 2019 · The 9M96E is a single-stage missile with a dual mode guiding system, radar active in the final phase and inertial with radio- control in the ...
  50. [50]
    The Performance of Semi-Active Radar Guided Missiles against Sea ...
    This model is used to evaluate the performance of a monopulse semi-active missile system against a sea skimming target.
  51. [51]
    SAMs with active radar homing - Defence and Freedom
    Apr 1, 2009 · A disadvantage to active radar homing compared to SARH on SAMs that I've seen a USN Sea Sparrow tech talk about is that it makes them ...
  52. [52]
    Taiwan's Air and Missile Defence. Part 2: Patriot PAC-2 and PAC-3
    Oct 9, 2024 · Unlike the TVM-guided PAC-2, the PAC-3 has an active radar-homing seeker and relies on both aerodynamic control surfaces and side-thrusters ...
  53. [53]
    It Came From Outer Space - Asian Military Review
    Jul 18, 2017 · ... Active Radar Homing (SARH) guidance took place between 1975 and 1985. ... guided missile with a Lightweight Exo-Atmospheric Projectile ...<|control11|><|separator|>
  54. [54]
    AIM-120 Advanced Medium-Range Air-to-Air Missile, US
    Sep 15, 2023 · It can carry an 18.1kg high-explosive blast fragmentation warhead to a maximum range of between 20nm to 30nm. AIM-120 AMRAAM variants. The AIM- ...
  55. [55]
    New AIM-120E Variant Of AMRAAM Air-To-Air Missile Hinted At By ...
    Apr 1, 2025 · The AIM-120D-3 version offers further improvements, including enhanced seeker ... AIM-120D evolved from a subvariant upgrade effort for the AIM- ...
  56. [56]
    [PDF] State Department Advanced Medium Range Air-to-Air Missile ... - DTIC
    The policy restricted the export of AMRAAM, but allowed continued export of the AIM-7 Sparrow, which like the AMRAAM is a beyond visual range air-to-air ...Missing: ITAR | Show results with:ITAR<|separator|>
  57. [57]
    AIM-7 Sparrow > Air Force > Fact Sheet Display - AF.mil
    The AIM-7 Sparrow is a radar-guided, air-to-air missile with a high-explosive warhead. The versatile Sparrow has all-weather, all-altitude operational ...Missing: variant | Show results with:variant
  58. [58]
    Raytheon AIM/RIM-174 Standard SM-6 - Designation-Systems.Net
    Jan 27, 2025 · The missile's active radar seeker takes over as soon as it can identify and track the target. The 64 kg (140 lb) blast-fragmentation warhead is ...Missing: homing | Show results with:homing
  59. [59]
    Canada Sends First NASAMS Air Defense System For Deployment ...
    Nov 5, 2024 · Canada's involvement in the NASAMS program dates back to 2023, when the country joined the United States in a joint order for the production ...
  60. [60]
    MICA - MBDA
    Specifications · Weight. 112kg · Length. 3.1m · Diameter. 160mm · Mission. Air Dominance · Platforms. Mirage 2000. Rafale ...Missing: active homing
  61. [61]
    ASTER 30 - MBDA
    ASTER 30 is for area protection, with quick reaction, 360º coverage, and high agility. It is part of the ASTER family, with a terminal dart.
  62. [62]
    METEOR - MBDA
    METEOR is the next generation Beyond Visual Range Air-to-Air Missile (BVRAAM) system designed to revolutionise air-to-air combat in the 21st century.
  63. [63]
    ASRAAM - MBDA
    Higher speed, combined with optimised aerodynamics create increased agility. This makes ASRAAM the best WVR missile available.Missing: ARH upgrades
  64. [64]
    The RBS15 family | Saab
    RBS15 is a highly optimized anti-ship missile with land attack capability, designed to give you the edge to stay ahead in increasingly complex conflict ...Missing: ARH | Show results with:ARH
  65. [65]
    Advanced IRIS-T Air-To-Air Missile _ As Of 2025 Updates - AirPra
    Apr 25, 2025 · The IRIS-T is a Fox-2 category missile featuring a Dual-Mode Seeker, which combines an Imaging Infrared Seeker and an Active Radar Seeker.
  66. [66]
    Cost-Effectiveness and Evolving Capabilities of the IRIS-T SLM and ...
    Aug 18, 2025 · In addition to extended range, the SLX variant incorporates a dual-mode seeker, combining active radar homing with imaging infrared guidance.
  67. [67]
    India firing up orders for its homegrown Astra missile - Asia Times
    Jun 9, 2022 · India awarded a US$424.4 million contract to state-run Bharat Dynamics Limited to supply the homegrown Astra Mk1 beyond-visual-range (BVR) air-to-air missile ...
  68. [68]
    India Targets 'Russian Customers' For Its Indigenous BVR Missiles
    Aug 22, 2024 · ... Astra is positioned as a superior alternative to the widely-used Russian R-77 missile. Vinod Kumar, General Manager of New Projects at BDL ...
  69. [69]
    PL-12 (AA-7A Adze) Chinese Air-to-Air Missile - ODIN
    May 30, 2025 · The PL-12 (AA-7A Adze) Chinese Air-to-Air Missile is an active radar-guided beyond-visual-range air-to-air missile developed by the People's Republic of China.Missing: homing introduction<|separator|>
  70. [70]
    PLA Air to Air Missiles - Air Power Australia
    China manufactures only two Beyond Visual Range (BVR) guided AAMs, the active radar guided PL-12/SD-10 “Sino-AMRAAM” and a reverse engineered semi-active radar ...
  71. [71]
    PL-15 air-to-air missile - Army Recognition
    The missile features an active electronically scanned array (AESA) radar seeker and a dual-pulse solid rocket motor, providing a range exceeding 200 kilometers.
  72. [72]
    PL-15 air-to-air missiles - ODIN - OE Data Integration Network
    Jun 17, 2024 · The missile features an active electronically scanned array radar, and has a range exceeding 200 km – comparable to that of the Russian R-37 missile.Missing: homing | Show results with:homing
  73. [73]
    HQ-9 - Missile Defense Advocacy Alliance
    Jun 20, 2018 · Modern HQ-9B interceptors use inertial guidance during flight and active radar homing during their terminal phase, enhancing the probability of ...
  74. [74]
    R-77 medium-range guided missile (RVV-AE) - Missilery.info
    Active radar homing. Country: Russia. Range: 80 km. Year: 1994. Similar in definition and basing: Short range airborne missile RVV-MD ...
  75. [75]
    R-77
    When the R-77 missile is at a distance of about 20 km its radar homing head activates leading the missile to its target.
  76. [76]
    R-37M (AA-X-13/AA-13 Arrow) Russian Air-to-Air Missile
    Jun 14, 2024 · The R-37M is a Russian supersonic, long-range air-to-air missile designed to attack C4ISTAR aircraft. It has a range exceeding 300km and is ...Missing: homing | Show results with:homing<|control11|><|separator|>
  77. [77]
    S-500 Prometey [Prometheus] - Components - GlobalSecurity.org
    Aug 25, 2021 · Active radar homing head (expected in 2012) to engage targets out of sight from the ground (for homing missile can) is designed to find the ...
  78. [78]
    The Air-To-Air Missiles That Equip India And Pakistan's Fighters
    May 8, 2025 · India selected the ASRAAM for its upgraded ... As such, the beyond-visual-range missile features active radar homing, as well as a datalink for ...
  79. [79]
    Astra Weapon System | Official Website of Bharat Dynamics Limited ...
    Range : 80 -110 km; Altitude : up to 20 km; Length : 3840 mm; Diameter ... Guidance : Inertial, mid-course update and terminal active radar homing (13 km) ...Missing: 2020 | Show results with:2020
  80. [80]
  81. [81]
  82. [82]
    XAAM-4 Medium Range Air-to-Air Missile Short ... - GlobalSecurity.org
    Dec 28, 2016 · As the XAAM-4 is based on an active radar homing system, the firing aircraft can fire several missiles independently to hit multiple targets ...
  83. [83]
    ASM Anti-Ship Missiles
    Jun 8, 2023 · Terminal Homing: To improve accuracy and target discrimination, these missiles often utilize terminal guidance systems such as active radar ...
  84. [84]
    Australia invests in new AIM-120 missile procurement - Janes
    Jul 4, 2025 · Canberra is investing up to AUD2.12 billion (USD1.3 billion) to procure additional stocks of AIM-120D-3 and AIM-120C-8 Advanced Medium-Range Air-to-Air ...
  85. [85]
    Mission success for Long Range Anti-Ship Missile testing
    Mar 21, 2025 · The LRASM is now ready for operational use after the operational test, which was conducted by Royal Australian Air Force (RAAF) F/A-18F Super ...
  86. [86]
    Hsiung Feng III - Missile Threat - CSIS
    The missile is propelled by a solid-fueled booster and liquid-fueled ramjet engine. The missile is guided by INS with terminal active radar homing. It is ...
  87. [87]
    South Korea enhances air defence shield with M-SAM improvements
    Aug 8, 2025 · The solid-fuel missile will achieve speeds of Mach 4.5, and use inertial guidance and active radar homing to address both short- and medium- ...
  88. [88]
    South Korea initiates Cheongung M-SAM enhancement - Janes
    Jul 31, 2025 · DAPA said the upgrade will “significantly strengthen our military's ballistic missile response capabilities”. It added that the Cheongung I ...Missing: 200K | Show results with:200K
  89. [89]
    Protecting the homeland: Accelerating ground-based air and missile ...
    Oct 23, 2025 · Develop a longer-term plan to produce either the AIM-120 AMRAAM family of missiles and/or the PAC-3 missile in Australia. ASCA and DSTG.