Experimental hypervelocity impacts: Implication for the analysis of material retrieved after exposure to space environment: Part I. Impacts on aluminium targets

During the last three decades a wide variety of surfaces have been brought back to Earth after being exposed to space environment. The impact features found on these surfaces are used to evaluate the damages caused to spacecraft and can give clues to the characteristics of the orbital debris and meteoroids that created them. In order to derive more precisely the particle parameters and to improve the analysis of projectile remnants, we have performed an extensive analysis of craters caused by the impact of high velocity particles on thick ductile targets, using a micro-particle accelerator. We show that from the geometry of the craters and from the analysis of the remnants it is possible to derive the main characteristics of the projectiles. In particular, using up-to-date instrumentation, scanning electron microscope (SEM) and Energy Dispersive X-ray (EDX) spectrometer, we found that even small residues inside craters can be identified. However, this study shows that a velocity resolution better than 1 km/s would be appropriate to obtain a fair calibration of the impact processes on a ductile target. This would allow to decipher with precision impact features on ductile surfaces exposed to space environment.

► Damages to spacecraft can be caused by the impact of micrometeoroids or space debris. ► High velocity impact produce perforation or craters depending on the nature or thickness of targets. ► Remnants of impacting particles can be found inside impacts craters and identified by SEM and EDX. ► Morphology and geometry of impact craters are used to assess the size of impacting particles. ► Analysis of material exposed to space environment provides clues about particulate space environment.