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Target drone

A target drone is an (UAV) designed primarily for training and weapons testing, simulating the flight characteristics of enemy , missiles, or other threats to allow safe practice for air defense systems without risking manned . These drones are typically radio-controlled or autonomous, expendable or recoverable, and equipped with features like reflectors, signatures, or towed targets to mimic real adversaries. The development of target drones traces back to , when the need for realistic gunnery practice spurred early innovations such as Britain's radio-controlled Aerial Target, tested in March 1917, and the ' Kettering Bug, an explosive-laden biplane that first flew in October 1918. During the , the British de Havilland DH.82B Queen Bee, a variant of the Tiger Moth trainer introduced in , became a foundational model for anti-aircraft training, popularizing the term "drone." accelerated production, with the U.S. mass-manufacturing nearly 15,000 target drones during the war, including over 9,400 units of the OQ-3 model, to train gunners and test systems, marking the shift from experimental to operational use. Postwar advancements incorporated jet propulsion and advanced guidance, exemplified by the (AQM-34) in the 1950s, which served as both a target and platform, logging over 34,000 missions. drones are categorized by scale and performance, including full-scale replicas like the QF-16 (a converted F-16 for threat ) and subscale models like the BQM-167A, which supports subsonic speeds up to 0.92 for air-to-air testing. In modern applications, they remain essential for evaluating missile accuracy, radar effectiveness, and counter-UAV defenses, with ongoing programs emphasizing cost-effective, high-fidelity simulations to address evolving aerial threats.

Overview and History

Definition and Purpose

A is an (UAV) designed to simulate enemy aircraft or missiles for training anti-aircraft and air defense personnel. These systems replicate real-world aerial threats, such as crewed , rotary-wing aircraft, or uncrewed systems, to enable realistic evaluation of military defenses. One early example is the 1917 British Aerial Target, a radio-controlled used for gunnery practice. The primary purposes of target drones include simulating aerial threats to train gunners, radar operators, and missile crews in detection, tracking, and engagement tactics. They also provide realistic targets for live-fire exercises, allowing testing of weapon systems' lethality and survivability without endangering manned or personnel. This approach supports congressional mandates for operational testing of defense capabilities, including air-to-air and surface-to-air munitions. Target drones are typically remote-controlled, either via ground stations or onboard programming, and can be recoverable for reuse or expendable depending on mission requirements. They often incorporate telemetry systems to transmit real-time performance data, such as flight parameters and sensor readings, facilitating post-mission analysis. The term "drone" originated in the 1930s from the British DH.82 Queen Bee, a radio-controlled biplane target variant of the de Havilland Tiger Moth that produced a buzzing sound akin to a bee; U.S. Navy officer Delmar Fahrney adopted the name to describe similar unmanned targets. Unlike reconnaissance or combat UAVs, which focus on intelligence gathering or offensive operations, target drones emphasize deliberate vulnerability to incoming fire for training efficacy and frequently include hit-detection mechanisms to score engagement accuracy.

Historical Development

The development of target drones began during , driven by the need for safer and more cost-effective alternatives to manned aircraft in training exercises. In 1917, British engineer Archibald Montgomery Low designed the Aerial Target, recognized as the first tested for military purposes, which demonstrated basic remote guidance capabilities though it was never used operationally. The following year, in 1918, the introduced the , an unmanned aerial torpedo developed by Charles Kettering for the U.S. Army Signal Corps, featuring preset flight paths via an onboard and to enable autonomous toward targets up to 75 miles away, though it saw limited testing before the war's end. During the , advancements in spurred more practical designs for gunnery practice. In 1935, the British introduced the DH.82 , a radio-controlled variant of the biplane, modified with a servo-assisted control system for takeoff, flight, and landing under remote operation, primarily to train naval anti-aircraft crews while reducing risks to human pilots. Over 400 units were produced, establishing it as a foundational model for reusable target drones and influencing the modern term "" derived from its name. World War II accelerated mass production and deployment of target drones amid escalating training demands. The U.S. Radioplane OQ-2, developed by Reginald Denny's company starting in the late 1930s, became the first mass-produced unmanned aerial vehicle, with approximately 15,000 units (including variants like the OQ-3) built from wood and fabric for the Army Air Forces by 1945, launched via catapult and controlled via ground radio to simulate enemy aircraft in gunnery and radar training. In Britain, the Fairey Queen, adapted from the Fairey IIIF floatplane in the early 1930s and refined for wartime use, served as a radio-controlled target for anti-aircraft exercises, with limited production of around three units that underwent successful gunnery trials by 1933. Post-World War II, the era marked a transition to higher-performance jet-powered systems, emphasizing recoverability and versatility. The , contracted by the U.S. Air Force in 1948 with its first flight in 1951, introduced subsonic jet propulsion using a Teledyne J69 engine, initially designed for target practice but later adapted for , and featured parachute recovery systems to enable reuse and data retrieval after missions. This shift was influenced by cost savings—drones were far cheaper than manned targets—and rapid progress in reliability and component miniaturization, allowing more complex flight profiles. From the 1970s onward, target drones incorporated advanced guidance like the U.S. Navy's BQM-74 Chukar, a subsonic jet model entering service in the mid-1970s with rocket-assisted launch and for monitoring during testing, building on earlier variants produced since 1965. The , starting in the 1980s, integrated GPS for precise navigation and enhanced for post-flight analysis, improving simulation of diverse threats in training. Lessons from the , where drones like the 147 series highlighted the value of unmanned systems in high-risk reconnaissance, further drove these innovations by underscoring the need for expendable yet recoverable assets to minimize personnel losses.

Design and Technology

Airframe and Propulsion

Target drones feature airframes designed to be lightweight and highly aerodynamic, closely mimicking the flight characteristics of manned to provide realistic training targets. Early models, such as the World War II-era , utilized inexpensive, disposable materials like wood and balsa for construction, enabling while maintaining structural integrity under stresses. Over time, materials evolved to include aluminum alloys for enhanced durability in high-speed impacts and modern composites such as and carbon fiber, which reduce weight and allow precise control over radar cross-sections for stealthier simulations. These material advancements have improved survivability during test environments, with composites offering superior strength-to-weight ratios compared to traditional metals. Target drone sizes and configurations vary widely to accommodate diverse simulation needs, ranging from compact radio-controlled models with 1-2 meter wingspans for low-altitude to full-scale conversions up to 12 meters for high-fidelity manned replication. Wing configurations are tailored to mission profiles, employing high-aspect-ratio designs in glider-like drones for extended endurance and , while delta or swept-wing shapes predominate in supersonic variants to achieve stable high-speed flight. For instance, the series adopts a straight-wing layout with a of approximately 3.9 meters, balancing maneuverability and speed. These configurations ensure aerodynamic efficiency, with fixed-wing dominance across most designs for sustained powered flight. Propulsion systems in target drones have transitioned from engines in early iterations to advanced and technologies, reflecting the need for higher performance in post-1950s applications. Initial models relied on engines producing 6-130 horsepower, driving propellers for speeds and economical operation in short-range exercises. By the mid-20th century, engines became standard, as exemplified by the Teledyne Ryan Firebee's Continental J69-T-29 delivering 1,700 pounds of thrust for velocities up to Mach 0.9. Solid-fuel s supplement these in select high-speed dash configurations, providing brief bursts to simulate threats without sustained power requirements. This evolution from to propulsion enabled the shift to faster, more versatile aerial targets. Performance parameters of target drones emphasize versatility in speed, altitude, and endurance to replicate a broad spectrum of threats. Typical operational speeds range from 100 to 600 knots, with ceiling altitudes reaching up to 50,000 feet in jet-powered models like the BQM-167A, which achieves 0.92 at . Endurance varies from 30 minutes in high-maneuverability rocket-assisted drones to over 8 hours in fuel-efficient variants designed for prolonged . Cost-effective launch methods, including towlines from manned or pneumatic catapults, facilitate deployment without onboard runways, enhancing logistical flexibility in training scenarios. To optimize transport and safety, target drones incorporate enhancements such as foldable wings for compact storage and pyrotechnic destruct mechanisms for controlled termination. Foldable wing designs, common in recoverable models, allow wingspans to collapse for easier shipping while maintaining aerodynamic performance upon deployment. Destruct systems employ explosive charges to fragment the mid-flight if control is lost, preventing uncontrolled debris hazards and ensuring mission safety in populated test ranges. These features underscore the balance between operational realism and practical recoverability in target drone engineering.

Avionics and Control Systems

Target drones rely on sophisticated avionics and control systems to enable remote operation, autonomous flight, and realistic threat simulation during military training and testing. Early systems primarily utilized line-of-sight radio control, as seen in the Radioplane OQ-2, which employed a Bendix radio control system for basic commands like throttle, rudder, and elevator adjustments, allowing operators to guide the drone from ground stations during antiaircraft gunnery practice. By the 1930s, British developments like the Fairey Queen IIIF Mk. IIIB incorporated radio control for converted biplanes, marking a shift toward more reliable wireless guidance over short ranges. The evolution to systems in the mid-20th century introduced datalinks using UHF and VHF frequencies for real-time transmission, enhancing beyond-visual-range control. For instance, the (BQM-34) series, introduced in 1951, integrated such datalinks with the System for Naval Target Control (SNTC), permitting operation up to 200 nautical miles while relaying flight data like position and speed. These advancements built on foundational gyroscopic stabilization from pioneers like Elmer Sperry in the , which provided early functions for maintaining level flight without constant manual input. Autopilot and navigation technologies progressed significantly with the adoption of inertial navigation systems (INS) in the 1950s, enabling drones to follow pre-set paths using gyroscopes and accelerometers for dead-reckoning without external references. The Firebee exemplified this by incorporating INS for autonomous recovery and maneuver execution, reducing operator workload during high-speed tests. Modern target drones integrate GPS-aided INS for precise, pre-programmed flight profiles, including evasive maneuvers such as high-g turns and low-altitude sea-skimming, as featured in Airbus's Do-DT55 with advanced navigation capabilities. As of 2025, advancements include AI-driven autonomy, as demonstrated in collaborative flights between Shield AI and Airbus using the DT25 target drone for enhanced independent operations in GPS-denied environments. This hybrid approach ensures robust performance in GPS-denied environments, where INS maintains accuracy for up to several hours of flight. Sensors play a critical role in monitoring and simulating threats, with telemetry pods transmitting on speed, altitude, and via datalinks to ground stations for immediate assessment. Advanced models, like the BQM-34, support video feeds from onboard cameras to provide operators with visual confirmation of maneuvers and engagement outcomes. suites enhance realism by incorporating countermeasures such as and dispensers, radar reflectors, and RF jammers; for example, the MQM-107B Streaker employs / pods and foam cone reflectors to mimic enemy electronic countermeasures during missile tests. systems further include (IR) flares and simulation payloads to replicate tactical threats like sea-skimming missiles. Recovery aids, such as radar altimeters, trigger deployment at low altitudes, ensuring safe retrieval after missions. Power systems for these avionics typically consist of onboard batteries or engine-driven s to supply servos, sensors, and transmitters, with designs prioritizing endurance for extended flights. The Firebee, for instance, uses a coupled to its for reliable power during supersonic runs. is emphasized in control surfaces, where dual servos for ailerons and rudders allow continued operation despite single-point failures, as in certified systems like the Do-DT series that meet airworthiness standards for high-g maneuvers. Post-flight analysis relies on black-box recorders, akin to flight data recorders in UAVs, which log parameters like inputs and sensor readings to evaluate test effectiveness and refine future scenarios.

Classification

Purpose-Built Drones

Purpose-built target drones are engineered specifically for use as expendable or recoverable aerial targets, emphasizing design principles that prioritize low production costs, disposability, and modular configurations to mimic diverse threat profiles without relying on modifications to platforms. This approach allows for high-volume and frequent deployment in training scenarios, where economic viability is critical. Early examples like the exemplified this philosophy through simplified construction using readily available components, such as a basic two-cylinder , to achieve at a of approximately $1,195 in 1943. in these systems facilitates the integration of interchangeable payloads, such as electronic countermeasures or signature enhancers, enabling simulation of various enemy behaviors while maintaining operational simplicity. Pioneering U.S. examples include the , introduced in the 1940s as a radio-controlled, propeller-driven for antiaircraft gunnery . Powered by a 6-horsepower, two-cycle in a , it achieved speeds up to 90 mph and altitudes of 8,000 feet, with launches from catapults and recovery via for reusability. Over 15,000 units were produced by 1945, making it the first mass-produced unmanned aerial system in the U.S. and a cornerstone for early air defense practice. The , developed in the , advanced this lineage with via a , offering speeds exceeding 600 mph, ranges up to 796 miles, and service ceilings of 60,000 feet; its recovery system, often aided by retrieval, supported extensive use from the through the in missile testing and pilot across U.S. branches. The , entering service in the mid-1960s, further refined subsonic target capabilities with a Williams engine, enabling zero-length launches from land or ships and maneuvers at low altitudes down to 7 feet. More than 1,600 units of the BQM-74C variant alone were produced for the U.S. Navy and , with the series emphasizing recoverability and high-volume output to support anti-ship and air-to-air exercises. These drones incorporate dedicated advantages such as customizable cross-sections through and optimizations to replicate specific threats, and integrated scoring systems with sensors that transmit real-time impact data for post-mission . allows multiple units to operate in swarms, simulating massed attacks and enhancing realism. Development trends in purpose-built target drones have progressed from and early designs to higher-performance variants, including supersonic models derived from canceled programs like the Regulus II missile in the 1950s, which were adapted into recoverable targets by adding for speeds exceeding Mach 1. These advancements underscore a shift toward versatile, cost-effective systems that balance disposability with technological sophistication for training. As of 2025, programs like the BQM-177A continue this evolution, providing supersonic threat simulation for advanced air defense testing.

Converted Aircraft

Converted aircraft target drones are created by adapting retired manned aircraft, typically fighters or bombers, into remotely controlled systems to simulate realistic threats during training and testing. The conversion process involves removing the cockpit or pilot seats to eliminate human occupancy risks, installing servo actuators on for remote manipulation, and adding telemetry antennas and onboard computers for real-time data transmission and command reception. Structural reinforcements are applied to the to withstand high-G maneuvers, often up to 9g, enabling aggressive evasion tactics that mimic adversary behavior. These modifications repurpose surplus airframes into reusable assets capable of autonomous takeoff, , and landing under ground control. Prominent examples include the U.S. QF-86 Sabre, derived from the North American F-86 jet fighter, with conversions beginning in the 1970s for both Army and use; the QF-86E variant served the U.S. Army from 1975 to 1996 as a target for supersonic training exercises. The QF-4 Phantom II, converted from McDonnell Douglas F-4 fighters starting in the late 1980s and continuing into the 1990s, represented a major program with over 300 units produced by 2016, primarily for testing at bases like . These conversions offer significant advantages, including the retention of the original 's realistic dimensions, speeds exceeding , and flight envelopes, which provide more authentic threat simulation than smaller purpose-built drones. Cost-effectiveness is achieved through reusing surplus airframes, with QF-4 conversions costing about $2.6 million each—far less than developing new platforms—while allowing the addition of mock and /infrared countermeasures to evaluate weapon systems comprehensively. This approach extends the service life of legacy , enabling them to carry simulated payloads for dynamic testing scenarios. Despite these benefits, challenges include maintenance difficulties from aging components and parts scarcity, compounded by safety risks in high-threat simulations where drones may be destroyed. The faced these issues, leading to its phase-out in 2016 after the final unmanned flight, with transitions to newer Full-Scale Aerial Target (FSAT) systems like the to address sustainment problems. As of 2025, the continues to provide high-fidelity threat representation. Internationally, the and nations converted MiG-15 and MiG-17 fighters into radio-controlled target drones post-1950s service, using them for air defense training across forces; these adaptations provided cost-effective, high-performance targets similar to practices.

Operational Applications

Military Training Exercises

Target drones play a crucial role in military training exercises by simulating realistic aerial threats, allowing personnel to practice interception and engagement tactics without risking manned aircraft. These drones replicate various scenarios, such as low-level attacks, formation flights, and high-altitude intercepts, enabling pilots and gunners to hone defensive skills in dynamic environments. For instance, in U.S. fleet exercises, target drones like the BQM-74 series are launched to integrate with live-fire gunnery practice, where surface-to-air missiles or aircraft weapons are fired against them to mimic anti-ship or defense operations. In skill development, target drones provide essential visual and audio cues for tracking and targeting, enhancing pilot and gunner proficiency in real-time decision-making. They support night operations through beacons or signatures, allowing training in low-visibility conditions critical for modern air defense. Evaluation during these exercises focuses on key performance indicators, such as response time to threat detection and engagement success rates, which inform tactical improvements across units. The U.S. employs drones like the BQM-167A in Weapons System Evaluation Program exercises to simulate high-maneuverability adversaries, achieving speeds up to 0.91 and pulls up to 9G for dogfight-like training. Exercises occur at large scales and regular frequencies to maintain readiness, with annual events involving dozens of drone sorties to test integrated force operations. The U.S. Army adapts target drones for ground-based air defense drills, such as missile live-fire exercises where drones serve as surrogate threats to validate interceptor accuracy against low-flying targets. Costs per vary by drone type but emphasize affordability for expendable use, supporting high-volume without excessive budgetary strain. Safety protocols are integral to these operations, including operations within over designated ranges to prevent civilian exposure, remote destruct commands via onboard flight termination systems to neutralize errant drones mid-flight, and post-exercise and to assess environmental and refine procedures. These measures ensure minimal risks while maximizing training realism, as demonstrated in and range activities.

Weapon Systems Testing

Target drones play a critical role in weapon systems testing by providing realistic, recoverable, or expendable platforms that simulate adversary , missiles, or other threats, enabling safe and controlled evaluation of munitions performance. These unmanned systems allow for live-fire trials of air-to-air missiles, surface-to-air missiles, anti-aircraft , and directed-energy weapons, replicating high-speed maneuvers, signatures, and profiles to assess targeting accuracy, lethality, and countermeasures effectiveness. In air-to-air testing, subscale aerial targets like the BQM-167A, developed by Composite Engineering Inc., support evaluations of fighter jet weapon systems by achieving speeds up to 0.92 and altitudes from 50 feet above ground level to 50,000 feet, with capabilities for 9G turns and integration of scoring systems, infrared enhancers, and pods. First flown in 2004 and achieving initial operating capability in 2008, the BQM-167A has been used in over 13 pre-operational flights to validate and impact dynamics. Similarly, full-scale aerial targets from Kratos Defense replicate threat-representative for missile development and pilot training, offering modular payloads and reusability to test end-to-end weapon integration while adapting to evolving threats. For surface-to-air and naval applications, high-speed target drones such as Airbus's Do-DT55neo simulate air-launched threats and sea-skimming missiles, reaching speeds of 100-485 knots and supporting infrared, radar, and laser training payloads for countering fast-moving targets. These systems have enabled over 3,500 missions worldwide, including tests of short-range infrared missiles via sub-target deployment from the Do-DT25. In a 2025 U.S. Navy demonstration, a BQM-34 target drone successfully air-launched a Solid Fuel Integral Rocket Ramjet (SFIRR) missile, validating propulsion integration and extending strike range from standoff positions while simplifying logistics with solid-fuel design. Such testing ensures weapon reliability under realistic conditions, with drones often incorporating , flares, and electronic countermeasures to evaluate system resilience, ultimately enhancing operational effectiveness without risking manned assets.

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