Survivability of copper projectiles during hypervelocity impacts in porous ice: A laboratory investigation of the survivability of projectiles impacting comets or other bodies

• Published in: Icarus (New York, N.Y. 1962) Vol. 268; pp. 102 - 117
• Main Authors: McDermott, K.H., Price, M.C., Cole, M., Burchell, M.J.
• Format: Journal Article
• Language: English
• Published: Elsevier Inc 01.04.2016
• Subjects: Comet Tempel-1; Comets; Cratering; Craters; Damage; DEFORMATION; Fragments; Hypervelocity impact; Impact processes; IMPACT PROPERTIES; Mars; Meteorites; POROSITY; PROJECTILES; SPACE VEHICLES; Survivability; Impact processes; Cratering; Mars; Meteorites; Comet Tempel-1
• ISSN: 0019-1035; 1090-2643
• DOI: 10.1016/j.icarus.2015.12.037

•Impacts of 1 and 2mm Cu spheres at up to 7.05kms−1 on porous ice are reported.•Fragments of Cu are found post shot in the wall and floor of the impact crater.•Between 1 and 2kms−1 the spheres are recovered intact with minor surface damage.•Between 2 and 2.5kms−1 the spheres are suffer increasing ductile deformation.•Above 2.6kms−1, the spheres fragment with increasing numbers of fragments. During hypervelocity impact (>a few kms−1) the resulting cratering and/or disruption of the target body often outweighs interest on the outcome of the projectile material, with the majority of projectiles assumed to be vaporised. However, on Earth, fragments, often metallic, have been recovered from impact sites, meaning that metallic projectile fragments may survive a hypervelocity impact and still exist within the wall, floor and/or ejecta of the impact crater post-impact. The discovery of the remnant impactor composition within the craters of asteroids, planets and comets could provide further information regarding the impact history of a body. Accordingly, we study in the laboratory the survivability of 1 and 2mm diameter copper projectiles fired onto ice at speeds between 1.00 and 7.05kms−1. The projectile was recovered intact at speeds up to 1.50kms−1, with no ductile deformation, but some surface pitting was observed. At 2.39kms−1, the projectile showed increasing ductile deformation and broke into two parts. Above velocities of 2.60kms−1 increasing numbers of projectile fragments were identified post impact, with the mean size of the fragments decreasing with increasing impact velocity. The decrease in size also corresponds with an increase in the number of projectile fragments recovered, as with increasing shock pressure the projectile material is more intensely disrupted, producing smaller and more numerous fragments. The damage to the projectile is divided into four classes with increasing speed and shock pressure: (1) minimal damage, (2) ductile deformation, start of break up, (3) increasing fragmentation, and (4) complete fragmentation. The implications of such behaviour is considered for specific examples of impacts of metallic impactors onto Solar System bodies, including LCROSS impacting the Moon, iron meteorites onto Mars and NASA’s “Deep Impact” mission where a spacecraft impacted a comet.