Momentum enhancement for the DART kinetic impactor
- Author(s)
- Thomas I. Maindl, Christoph M. Schäfer
- Abstract
We study kinetic impacts of a spacecraft as an option to deflect sub-kilometer sized potentially hazardous asteroids that may collide with Earth. Near-Earth asteroids of this size are difficult to observe and at the same time are believed to be very common and to consist of a wide variety of materials with varying bulk densities. The momentum delivered by such an impact of a spacecraft may alter the asteroid's orbit and henceforth avoid an impact with our home world. In addition to a direct transfer of momentum from the projectile to the target, a kinetic impact will also involve post-impact effects caused by material ejected from the impact site. This will result in a momentum transfer efficiency beta greater than 1 which is only weakly constrained. Thriving for constraining this beta factor, we investigate the impact of a spacecraft onto an asteroid similar in size to the secondary body of the binary near-Earth asteroid (65803) Didymos, the target of NASA's Double Asteroid Redirection Test (DART) and ESA's Hera mission concepts. We present results from simulations with our own 3D smooth particle hydrodynamics (SPH) hypervelocity impact code. Depending on the impact angle and target porosity, we find beta factors between 1.15 and 1.93, which is compatible with results obtained in a previous study and by others using various methods.
- Organisation(s)
- Department of Astrophysics
- External organisation(s)
- Eberhard Karls Universität Tübingen
- Volume
- 13
- Publication date
- 09-2019
- Austrian Fields of Science 2012
- 103003 Astronomy, 103004 Astrophysics
- Portal url
- https://ucrisportal.univie.ac.at/en/publications/a26b925c-2e31-4253-9d0b-576d4cdeab3d