Radiation Pressure Calculator

Calculate radiation pressure, force, and acceleration from electromagnetic radiation on absorbing or reflecting surfaces. Solar sail and laser propulsion analysis.

W/m²
kg
Radiation Pressure
4.5398e-6 Pa
4.540e+0 µPa
Force on Surface
4.5398e-6 N
4.540 µN
Acceleration
4.5398e-6 m/s²
Mass = 1.00 kg
ΔV per Day
3.922e-1 m/s
Continuous illumination
Speed after 1 Year
143.27 m/s
0.143 km/s
Irradiance
1,361.0 W/m²
Area = 1.0000 m²

Force vs Distance from Sun

Mercury orbit
0.5 AU
Venus
Earth
Mars
Jupiter
Saturn
Neptune
Kuiper belt
LocationAUI (W/m²)P (Pa)F (N)a (m/s²)
Mercury orbit0.315,122.25.044e-55.044e-55.044e-5
0.5 AU0.55,444.01.816e-51.816e-51.816e-5
Venus0.722,625.48.757e-68.757e-68.757e-6
Earth11,361.04.540e-64.540e-64.540e-6
Mars1.52589.11.965e-61.965e-61.965e-6
Jupiter5.250.31.679e-71.679e-71.679e-7
Saturn9.515.15.030e-85.030e-85.030e-8
Neptune301.55.044e-95.044e-95.044e-9
Kuiper belt500.51.816e-91.816e-91.816e-9
Planning notes, formulas, and examples

About the Radiation Pressure Calculator

Radiation pressure is the force per unit area exerted by electromagnetic radiation on a surface. Maxwell's theory predicts P = I/c for a perfectly absorbing surface and P = 2I/c for a perfect reflector, where I is the irradiance (power per unit area) and c is the speed of light. Though tiny in everyday terms — about 4.6 micropascals for sunlight at Earth — radiation pressure has profound effects on dust grains, comet tails, spacecraft orbits, and proposed solar sail missions.

This calculator computes the radiation pressure, total force, and resulting acceleration for any surface area, irradiance, and object mass. Three surface modes are supported: perfect absorption, perfect reflection, and partial reflectivity with a user-specified coefficient. Presets include sunlight at various solar-system distances, focused laser beams, and solar sail concepts.

The distance table shows how solar radiation pressure drops as 1/r² from the Sun, illustrating why solar sails are most effective in the inner solar system. The delta-V accumulation over time — despite the tiny force — highlights why radiation pressure is a viable propulsion concept for long-duration missions.

When This Page Helps

Use this calculator when you want to translate irradiance into a physically meaningful force on a sail, mirror, or spacecraft.

It is useful for solar sail intuition, satellite perturbation estimates, laser-push concepts, and showing how a very small pressure can still produce measurable velocity over long missions. It also helps compare how area, reflectivity, and mass trade against one another in low-thrust mission concepts.

How to Use the Inputs

  1. Enter the irradiance (power per unit area) in W/m², or click a preset.
  2. Select the surface type: absorbing, reflecting, or partially reflective.
  3. For partial reflectivity, enter the reflectivity R (0 = absorbing, 1 = reflecting).
  4. Enter the surface area with unit (m², cm², or km² for solar sails).
  5. Enter the object mass in kg.
  6. Read the radiation pressure, total force, acceleration, and accumulated ΔV.
  7. Use the solar-system distance table to see how force varies from Mercury to the Kuiper belt.
Formula used
Absorbing surface: P = I / c Reflecting surface: P = 2I / c Partial reflectivity: P = I(1 + R) / c Force: F = P × A Acceleration: a = F / m Where: • I = irradiance (W/m²) • c = 299,792,458 m/s (speed of light) • R = reflectivity (0–1) • A = surface area (m²) • m = mass (kg)

Example Calculation

Result: P = 9.08 µPa, F = 9.08 mN, a = 9.08×10⁻⁴ m/s²

P = 2 × 1361 / 3×10⁸ = 9.07×10⁻⁶ Pa. F = 9.07×10⁻⁶ × 1000 = 9.07×10⁻³ N. a = 9.07×10⁻³ / 10 = 9.07×10⁻⁴ m/s². Over one year, this adds ~28.6 km/s — enough to escape the solar system.

Tips & Best Practices

  • For solar sail design, the key figure of merit is area-to-mass ratio (A/m). Higher A/m means higher acceleration.
  • Sunlight irradiance scales as 1/r² — moving to 0.5 AU quadruples the pressure.
  • Space agencies model SRP with a cannonball coefficient Cr ≈ 1.0–2.0 depending on spacecraft reflectivity and shape.
  • At distances beyond ~5 AU, radiation pressure becomes too weak for practical solar sailing.
  • For laser propulsion, beam divergence limits the effective range — the Rayleigh length sets the focusing distance.

Practical Guidance

Radiation pressure is most useful when you frame it in terms of area-to-mass ratio and exposure time. The instantaneous force is tiny, but spacecraft with very large reflective area and low mass can accumulate meaningful velocity over months or years without expending propellant. That is why the pressure value alone is less informative than the resulting acceleration and long-duration delta-V.

Common Pitfalls

The most common mistake is treating irradiance as constant regardless of distance or beam geometry. Solar flux falls with the inverse square of distance, and laser concepts are limited by beam divergence and pointing. Surface reflectivity also matters: a real sail sits somewhere between perfect absorption and perfect reflection.

Sources & Methodology

Last updated:

Frequently Asked Questions

  • Sunlight at Earth exerts only 4.56 µPa on a black surface and 9.12 µPa on a mirror. This is about 10 billion times smaller than atmospheric pressure. Yet over large areas and long times, it accumulates to measurable forces.