Calculate radiation pressure, force, and acceleration from electromagnetic radiation on absorbing or reflecting surfaces. Solar sail and laser propulsion analysis.
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.
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.
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)
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.
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.
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.
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.
Yes. JAXA's IKAROS (2010) demonstrated solar sailing. A 10 kg sail with 1000 m² area at 1 AU accelerates at ~0.9 mm/s². Over months, this builds up km/s of delta-V without fuel.
A perfect reflector reverses the photon momentum, giving 2p per photon (impulse = incoming + reflected momentum). An absorber only captures p. So reflection doubles the pressure.
Yes. Solar radiation pressure is a significant perturbation for high area-to-mass ratio satellites (e.g., GPS, geostationary). Attitude control must account for the torque, and orbit determination models include SRP.
Focused laser beams can deliver much higher irradiance than sunlight. Breakthrough Starshot proposes using a 100 GW laser array to accelerate gram-scale probes to 20% of light speed. This calculator shows the fundamental pressure relationship.
Sunlight pushes dust grains away from the comet nucleus. The dust tail always points away from the Sun because radiation pressure exceeds the Sun's gravity for micron-sized particles.