Asteroids are the smallest bodies in the solar system, usually with diameters on the order of a few hundred's, or even only tens of kilometers. The total mass of all asteroids in the solar system must be less than the mass of the Earth's Moon. Despite this fact, they are objects of great importance. They must contain information about the formation of the solar system, since its chemical and physical compositions remain practically constant over time. These bodies also pose a danger to Earth, as many of these bodies are on a trajectory that passes close to Earth. There is also the possibility of mining on asteroids, in order to extract precious metals and other natural resources. The present work aims to study the use of a kinetic impact technique as a way to deflect asteroids that may present some risk of collision with the Earth at a given time. This is a very current topic of research and it is related to planetary defense. It has been receiving the attention of researchers worldwide. In the work to be developed here, intend to evaluate in more detail the possibility of deflecting the orbit of asteroid 101955 Bennu, taking into account specific aspects. For this it, we used velocity variations simulating an impact opposite to the direction of the asteroid's movement (∆v∆v∙v negative) and also in the same direction of movement of the asteroid (∆v∆v∙v positive). The variations used here were from 10 mm/s to 50 mm/s. We also divided the impact point into 16 parts of the asteroid's orbital period, approximately 27 days to achieve greater precision in the results and also to reach the perihelion and aphelion points. We are also monitoring the influence of all planets in the solar system, applying the technique of deflecting the asteroid considering all the planets of the solar system, a system of 4 bodies (∆v Sun, Earth, Moon and asteroid) and a system of 5 bodies (∆v Sun, Earth, Moon, Jupiter and asteroid), to determine Jupiter's influence on the results. We are using the numerical integrator package Mercury N-bodies, designed to simulate the orbit of bodies of different sizes around a central body. The different numerical integrators present in Mercury allow the user to obtain a good relationship between the computational cost and the resolution of the simulations. Mercury also allows the user to add forces from sources other than gravity, as well as to modify algorithms such as collisions that, by default, result in the perfect fusion of two bodies with mass conservation and linear momentum.
AAS/Division of Dynamical Astronomy Meeting
- Pub Date:
- August 2020