Momentum and Angular Momentum Transfer in Oblique Impacts: Implications for Asteroid Rotations

• Published in: Icarus (New York, N.Y. 1962) Vol. 123; no. 1; pp. 192 - 206
• Main Authors: Yanagisawa, Masahisa, Hasegawa, Sunao, Shirogane, Nobutoshi
• Format: Journal Article
• Language: English
• Published: Elsevier Inc 01-09-1996
• ISSN: 0019-1035; 1090-2643
• DOI: 10.1006/icar.1996.0149

We conducted a series of high velocity oblique impact experiments (0.66–6.7 km/s) using polycarbonate (plastic) projectiles and targets made of mortar, aluminum alloy, and mild steel. We then calculated the efficiencies of momentum transfer for small cratering impacts. They are η = (M′Vn′)/(mvn) and ζ = (M′Vt′)/(mvt), wheremandvare the mass and velocity of a projectile, andM′ andV′ represent those of a postimpact target. Subscripts “n” and “t” denote the components normal and tangential to the target surface at the impact point, respectively. The main findings are: (1) η increases with increasing impact velocity; (2) η is larger for mortar than for ductile metallic targets; (3) ζ for mortar targets seems to increase with the impact velocity in the velocity range less than about 2 km/s and decrease with it in the higher velocity range; (4) ζ for the aluminum alloy targets correlates negatively with incident zenith angle of the projectile. In addition to these findings on the momentum transfer, we show theoretically that “ζL” can be expressed by η and ζ for small cratering impact. Here, ζLis the spin angular momentum that the target acquires at impact divided by the collisional angular momentum due to the projectile. This is an important parameter to study the collisional evolution of asteroid rotation. For a spherical target, ζLis shown to be well approximated by ζ.