Light scattering model for small space debris particles

We have developed a scattering model allowing to study interaction of light with particles populating the near-Earth environment: satellite explosion remnants, collisional debris, particles detached from peeling paint surfaces, and ejecta resulting from micrometeorite bombardment. In its present configuration the model accounts for rough needles, grains, and plates as primary shape elements. More complex shapes are built upon combining them. The model is compared and validated against laboratory measurements. The studied samples include a set of space debris analogue samples obtained from the controlled MIRAD (Microparticle impact related attitude disturbances) experiment that collided solar cell panels with a projectile. The resulting samples are mostly carbon needles and curved aluminium sheets. We have both measured and modelled the scattering of light from a set of these samples. The model agrees rather well with the measurements. The shape and orientation of the particles are found to be the main contributor in how light is scattered, whereas the material dependence shows a weaker trend. Large amount of data with varying viewing and illumination angles are needed to allow for inversion of the target characteristics. The experimental results exploited in our study have significantly aided the model development. In the future, this work can be expanded to a real-mode in-orbit scattering model that can be utilised in Earth system and/or astronomical observations and space mission concept designs. Additional measurements with larger variety of samples and their expanded size range are required to extend and solidify the model for the full range of populations representing space particles