Radar Range Equation Calculator

Solve the radar equation for maximum detection range, received power, or required transmit power. Includes RCS, system losses, and integration gain.

Calculator Electronics Updated Apr 23, 2026
How to Use
  1. Enter TX power, antenna gain, frequency, target RCS, RX sensitivity, and system losses.
  2. Result: maximum detection range under given SNR requirement.
Input
W
dBi
MHz/GHz
dBm
dB
Presets
Range Profile
Max Range
km
Wavelength
mm
EIRP
dBW
Round-Trip
µs

Show Work

Enter radar parameters.

Formulas

Radar Equation
R4 = P_t·G²·λ²·σ / ((4π)³·P_min·L)
Classic monostatic radar.
Inverse 4th root
R ∝ P_t^(1/4)
16× power → 2× range.
In dB
40·log(R) = P_t + 2·G + 20·log(λ) + σ − P_min − L − 33
Logarithmic form.
RCS Examples
F-22 ≈ 0.0001 · Cessna 5 · Truck 200
m² reference.
Round-Trip Time
t = 2R/c
6.67 µs/km round-trip.
Integration
+10·log(N) dB gain
N coherent pulses summed.

History of the Radar Equation

The radar equation was developed by Sir Robert Watson-Watt\'s team at the UK Air Ministry Research Establishment in 1935 as they designed the Chain Home radar system. The classic monostatic form — R⁴ = (P_t·G²·λ²·σ) / ((4π)³·P_min·L) — has remained unchanged in form since the 1940 MIT Rad Lab\'s formalization.

The fourth-root dependence on power is why radar development focused so heavily on higher antenna gain (G² in the equation, so doubling gain gives 41% more range) rather than more transmitter power (which gives only 19%). WWII-era radar saw antenna diameters grow from 3m (Chain Home) to 10m+ by 1945 — a 4× improvement in area and 16× in effective power-range product.

Modern radars push the equation in different directions: AESA phased-array antennas (electronic beam steering, no mechanical gimbal), ultra-low-noise receivers (cryogenic amplifiers for deep-space), and pulse-compression techniques that trade time-bandwidth for SNR. But the underlying equation is still the one from 1940.

About This Calculator

Enter transmitter power (W), monostatic antenna gain (dBi — same antenna for TX and RX), frequency, target radar cross section (σ in m²), receiver minimum detectable signal (dBm), and system losses (dB). The tool solves R⁴ = P_t·G²·λ²·σ / ((4π)³·P_min·L) for the maximum detection range.

For bistatic radars (separate TX and RX antennas), or for integrating N pulses, modify inputs accordingly (2G → G_tx + G_rx; add +10·log(N) to sensitivity for integration gain). For monostatic pulse radars without integration, this is the standard equation. Everything runs client-side.

Frequently Asked Questions

What is RCS?

Radar Cross Section: the effective area of a target as seen by radar. A sphere of area A has RCS = A; a flat-plate reflector is much larger; stealth aircraft minimize RCS to < 0.01 m².

Why fourth root?

Signal travels out (r²) and back (r²), so round-trip energy falls as 1/r⁴. Doubling TX power only adds 19% range (2^(1/4) = 1.19).

What is integration gain?

Summing multiple pulses improves SNR. N coherent pulses: +10log(N) dB gain. 100 pulses = 20 dB effective sensitivity improvement.

Common Use Cases

Airport Radar

10 MW peak at S-band, 40 dB antenna, 1 m² target RCS: ~200 km range.

Automotive Radar

1 W at 77 GHz, 25 dB gain, 10 m² RCS: ~250 m range.

Weather Radar

Nexrad WSR-88D: 750 kW, 45 dBi, 0.01 m² RCS (raindrop): ~200 km.

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