Electronic Warfare and Signal Intelligence Practical EW Questions Informational

How do I design a wideband antenna for a radar warning receiver covering 2 to 18 GHz?

Designing a wideband antenna for a radar warning receiver covering 2 to 18 GHz (a 9:1 bandwidth ratio) requires an antenna that maintains consistent gain, polarization, and pattern across this extremely wide frequency range. The antenna must also provide direction-finding capability (amplitude or phase information for AoA measurement). The primary antenna types used are: cavity-backed spiral antenna (the most common RWR antenna; a planar spiral (Archimedean or equiangular) mounted over a metallic cavity with absorber loading; provides: 9:1+ bandwidth (2-18 GHz readily achievable), circular polarization (intercepts any linearly polarized threat signal with at most 3 dB loss), moderate gain (3-7 dBic across the band), and a broad, stable beam pattern (60-90 degree beamwidth, providing wide angular coverage); typical size: outer diameter approximately 75 mm for 2 GHz low-frequency cutoff), sinuous antenna (a four-arm variant of the spiral; provides dual-circular-polarization capability (simultaneous RHCP and LHCP) for more accurate DF; bandwidth: 10:1+ achievable; used in advanced DF systems), and ridged horn antenna (a horn antenna with ridged waveguide loading for ultra-wideband operation; provides: moderate gain (3-10 dBi), linear polarization, and very wide bandwidth (2-18 GHz); used when gain is more important than CP capability). For 360-degree azimuth coverage: 4-6 antennas are arranged around the platform (forward, aft, left, right, and optionally up and down). The amplitude comparison between antennas provides the AoA measurement.
Category: Electronic Warfare and Signal Intelligence
Updated: April 2026
Product Tie-In: Wideband Receivers, Amplifiers, Antennas

RWR Wideband Antenna Design

The RWR antenna is a critical component whose performance directly impacts the system's sensitivity, AoA accuracy, and probability of intercept.

  1. Performance verification: confirm specifications against the application requirements before finalizing the design
  2. Environmental factors: temperature range, humidity, and vibration affect long-term reliability and parameter drift
  3. Cost vs. performance: evaluate whether the application demands premium components or standard commercial grades
  4. Interface compatibility: verify impedance, connector type, and mechanical form factor match the system architecture
  5. Margin allocation: include sufficient design margin to account for manufacturing tolerances and aging effects
Common Questions

Frequently Asked Questions

Why circular polarization?

Threat radars can be: horizontally polarized (most ground-based surveillance radars), vertically polarized (some naval radars, some missile seekers), or slant-polarized (some fighter radars). A linearly polarized RWR antenna would suffer 3 dB loss when receiving a cross-polarized signal and potentially 20+ dB loss when perfectly cross-polarized. A circularly polarized spiral antenna receives any linearly polarized signal with at most 3 dB loss (since any linear polarization decomposes into equal RHCP and LHCP components, and the spiral captures one). This polarization-independent reception ensures that the RWR detects threat signals regardless of their polarization.

How is the AoA determined?

Amplitude comparison DF: the RWR has 4-6 antennas pointing in different directions (typically 60-90° beamwidth each). The same pulse is received by multiple antennas at different amplitudes. The antenna with the highest amplitude indicates the approximate bearing. The amplitude ratios between adjacent antennas provide a more precise bearing estimate: AoA = f(amplitude_1, amplitude_2, ... amplitude_N). Accuracy: ±5-15° (adequate for threat warning and countermeasure cueing). For more precise DF: use an interferometric approach (phase comparison between antennas) for ±1-5° accuracy. This requires coherent receivers on each antenna.

What about conformal antennas?

For aircraft: the RWR antennas must be conformal (flush-mounted on the aircraft skin) to avoid aerodynamic drag. Conformal spiral antennas: the spiral is printed on a flexible substrate and conformed to the aircraft surface curvature. The curvature affects the pattern (distorting the beam shape and shifting the phase center), but: for the broad beamwidths used in RWR (60-90°), moderate conformal distortion is acceptable. Blade antennas: some RWR installations use small blade antennas (protruding a few cm from the skin) that provide omnidirectional coverage but lower gain. The blade's small size limits the low-frequency coverage.

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