Radar Parameters
Transmitter
Antenna
dBi
Target
σ = 1 m² ≈ medium aircraft  ·  Click table below ↓
Receiver & System
dB
dB
dB
pulses
Results
Max Detection Range
Received SNR @ target range
Noise Power in Bandwidth
Min Detectable Signal (MDS)
Received Power @ Rmax
Pulse Bandwidth B
Radar Link Budget
ParameterValueNotes
Range vs Transmitted Power — at fixed SNR threshold
📋 Typical RCS Values — Click to Load
TargetTypical RCS σdBsmNotes
🐦 Bird / small UAV0.0001 m²−40 dBsmVery low RCS target
🛸 Small drone (DJI-size)0.01 m²−20 dBsmCounter-UAS challenge
🚶 Person (walking)0.05–0.5 m²−13 to −3 dBsmDepends on aspect angle
🏎 Small car1 m²0 dBsmSide aspect
🚗 Car / SUV (front)10 m²+10 dBsmFront/rear aspect
🛩 Small aircraft (GA)0.5–2 m²−3 to +3 dBsmGeneral aviation
✈️ Commercial aircraft10–100 m²+10 to +20 dBsmBroadside aspect
🥷 Stealth aircraft (F-22)~0.001 m²−30 dBsmClassified, approximate
🚢 Large ship1000–100000 m²+30 to +50 dBsmDepends on aspect
🛥 Small boat100 m²+20 dBsmTypical for marine radar
🚁 Helicopter0.3–3 m²−5 to +5 dBsmRotating blades modulate
🚂 Train (broadside)~400 m²+26 dBsmLarge metallic structure
Received SNR vs Target Range

About the Radar Range Calculator

This calculator implements the monostatic radar range equation — the fundamental formula that determines how far a radar system can detect a target of given radar cross section (RCS). It accounts for transmit power, antenna gain, wavelength, target RCS, noise figure, required SNR, and system losses.

The Radar Range Equation

The received power from a target at range R in a monostatic radar (same antenna for TX and RX) is:

Pr = Pt · Gt · Gr · λ² · σ · n / [(4π)³ · R⁴ · Lsys]
Solving for maximum range Rmax:
Rmax = [ Pt · G² · λ² · σ · n / ((4π)³ · k·T₀·B·NF · SNRmin · L) ]^(1/4)
where k = 1.38×10⁻²³ J/K (Boltzmann), T₀ = 290 K, B = 1/τ (matched filter), n = pulses integrated

Key Parameters

Radar Cross Section (RCS, σ) — the effective "mirror area" of the target. A larger RCS means more signal bounces back to the radar. RCS depends on target size, shape, material, and the aspect angle. Stealth aircraft use shaping and radar-absorbent material (RAM) to minimise RCS.

System Losses (L) — includes atmospheric absorption, radome insertion loss, waveguide losses, mismatch losses, and signal processing losses. A typical value for X-band radar is 4–10 dB total.

Pulse Integration (n) — coherently integrating n pulses improves SNR by n times (10·log₁₀(n) dB). Non-coherent integration improves SNR by approximately √n. This calculator assumes coherent integration.

The R⁴ Dependence

Notice the range appears as R⁴ in the denominator — this is the crucial difference between radar and one-way communication. The signal travels to the target (R² loss) and back (another R² loss). This means doubling the transmit power only increases range by 19% (2^(1/4) = 1.189). To double the radar range, you need 16× more transmit power — which is why radar engineers obsess over every dB.

Minimum Detectable Signal (MDS)

The MDS is the weakest signal the radar receiver can distinguish from noise. It equals the thermal noise floor raised by the noise figure and the required SNR: MDS = k·T₀·B·NF·SNRmin·L. Any received signal below MDS will be buried in noise and undetectable.