If considering one gram of steel and one gram of foam, which one is the biggest threat and would cause most or least damage to the orbital structure it hits?
Radii of these debris is the only thing that will differ, yet depending on impact velocity, damage should differ too.
How does relation between relative impact velocity and damage caused by impact evolve for the gram of steel and the gram of foam, since there is a wide range of possible impact velocities?
(for instance at 15 km/s (prograde vs retrograde LEO frontal impact) the foam should punch a bigger hole in a solar panel or a hull.
At 0.1 km/s the steel may produce a small bump on a hull while the foam may do nothing).