Electronic Warfare and Signal Intelligence Practical EW Questions Informational

How do I design a towed decoy system for aircraft self-protection against radar guided missiles?

Designing a towed decoy system for aircraft self-protection against radar-guided missiles creates a towed body connected to the aircraft by a thin cable (typically fiber-optic) that carries the threat radar's signal to the decoy, which amplifies and retransmits it to attract the missile away from the aircraft. The system consists of: the towed body (a small aerodynamic body, typically 10-30 cm long, containing: an RF amplifier/DRFM that receives the threat radar signal via the fiber-optic tow cable, amplifies it, and retransmits it from the towed body's antenna; the retransmitted signal appears to come from the towed body's location, 50-200 m behind the aircraft), the fiber-optic tow cable (a thin (1-3 mm diameter) Kevlar-reinforced fiber-optic cable, 50-200 m long; the fiber carries: the RF signal from the aircraft to the towed body (downlink) and power to the towed body (via a miniature generator or battery in the towed body, or via electrical conductors in the cable); the fiber-optic cable does not radiate RF and is invisible to radar), and the launch/recovery mechanism (a reel system on the aircraft that deploys the towed body in flight and reels it back when the threat is cleared; the system must deploy quickly (less than 10 seconds) and withstand the aerodynamic forces at the aircraft's operational speed (Mach 0.6-2.0)).
Category: Electronic Warfare and Signal Intelligence
Updated: April 2026
Product Tie-In: Wideband Receivers, Amplifiers, Antennas

Towed Decoy System Design

The towed decoy is one of the most effective countermeasures against modern radar-guided missiles because: it creates a physically separated false target (the missile detonates at the towed body's location, missing the aircraft by the tow distance), and it operates continuously (unlike expendable decoys that are one-shot).

  • Performance verification: confirm specifications against the application requirements before finalizing the design
  • Environmental factors: temperature range, humidity, and vibration affect long-term reliability and parameter drift
  • Cost vs. performance: evaluate whether the application demands premium components or standard commercial grades
Common Questions

Frequently Asked Questions

What towed decoy systems are in service?

AN/ALE-55 (Raytheon): fiber-optic towed decoy for F/A-18E/F Super Hornet. Uses a DRFM to generate coherent jamming from the towed body. The most advanced towed decoy in US service. AN/ALE-50: an earlier, simpler expendable towed decoy (not recovered). Used on B-1B, F-16. Ariel (Leonardo): towed decoy for European fighters (Eurofighter, Gripen). Sky Buzzer (Elbit Systems): Israeli towed decoy system. These systems are closely guarded technology; detailed specifications are classified.

What are the limitations?

Single-threat direction: the towed decoy trails behind the aircraft. It is most effective against threats approaching from behind or the sides. For head-on threats: the decoy is behind the aircraft and may not be in the missile seeker's beam. Maneuver constraints: the tow cable limits the aircraft's maneuver (sharp turns can stress or break the cable). Cable management: the cable must not tangle with the aircraft's control surfaces, engines, or weapons stations. Limited number: typically one towed decoy deployed at a time (some systems carry 2-3 decoy bodies for sequential deployment). Vulnerability: the cable can be cut by fragments from a near-miss, and the towed body can be shot down.

How does it work against a monopulse seeker?

A monopulse radar seeker measures the angle to the target in a single pulse (no conical scan or sequential lobing). It tracks the angular centroid of all returns within its beam. When both the aircraft and the towed decoy are in the seeker's beam: the centroid is pulled toward the stronger signal. If the decoy's effective RCS is 6+ dB above the aircraft: the centroid moves toward the decoy, and the missile tracks toward the decoy. The physical separation between the decoy and the aircraft means the missile detonates at the decoy's location, missing the aircraft. This is the primary mechanism by which towed decoys defeat modern monopulse-guided missiles.

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