Radar Range Equation

Rmax = (Pt×Gt×Gr×λ²×σ / ((4π)³×Smin))^0.25

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Result

Formula

R_max = (P_t × G_t × G_r × λ² × σ / ((4π)³ × S_min))^(1/4)

Description

The radar range equation determines the maximum detection range of a radar system. The transmitted power spreads over a sphere (1/R²), reflects off the target (with radar cross section σ), spreads again on the return path (another 1/R²), and must exceed the receiver minimum detectable signal. The fourth-root dependence means that doubling the range requires 16× the transmit power. This equation is fundamental to radar system design for military, weather, aviation, automotive, and maritime applications.

Variables

  • P_t — Transmitter peak power (W)
  • G_t — Transmit antenna gain (linear, not dB)
  • G_r — Receive antenna gain (linear, not dB)
  • λ — Wavelength (m)
  • σ — Target radar cross section (m²)
  • S_min — Minimum detectable signal power (W)

Practical Notes

Typical radar cross sections: bird 0.01 m², person 1 m², car 10-200 m², aircraft 1-100 m², ship 1000-100000 m². Antenna gains must be in linear (not dB): G_linear = 10^(G_dB/10). The equation assumes free-space propagation; atmospheric attenuation, multipath, and clutter reduce actual range. To convert S_min from dBm: S_min_W = 10^((dBm-30)/10).

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