Details

Autor(en) / Beteiligte

• Yu, Yang
• Michel, Patrick
• Schwartz, Stephen R.
• Naidu, Shantanu P.
• Benner, Lance A.M.

Titel

Ejecta cloud from the AIDA space project kinetic impact on the secondary of a binary asteroid: I. mechanical environment and dynamical model

Ist Teil von

• Icarus (New York, N.Y. 1962), 2017-01, Vol.282, p.313-325

Ort / Verlag

Elsevier Inc

Erscheinungsjahr

2017

Quelle

Access via ScienceDirect (Elsevier)

Beschreibungen/Notizen

• •This paper aims at an understanding of the ejecta cloud dynamics, which is crucial to the planning of the ongoing AIDA mission.•An informative dynamic model has been built to synthesize all relevant forces based on comprehensive analysis.•A full-scale simulation was organized towards the response of Didymos to DART impact and the following month-long evolution of the ejecta cloud.•Some interesting results about the post-impact physics have been uncovered according to the simulation. An understanding of the post-impact dynamics of ejecta clouds are crucial to the planning of a kinetic impact mission to an asteroid, and also has great implications for the history of planetary formation. The purpose of this article is to track the evolution of ejecta produced by AIDA mission, which targets for kinetic impact the secondary of near-Earth binary asteroid (65803) Didymos on 2022, and to feedback essential informations to AIDA’s ongoing phase-A study. We present a detailed dynamic model for the simulation of an ejecta cloud from a binary asteroid that synthesizes all relevant forces based on a previous analysis of the mechanical environment. We apply our method to gain insight into the expected response of Didymos to the AIDA impact, including the subsequent evolution of debris and dust. The crater scaling relations from laboratory experiments are employed to approximate the distributions of ejecta mass and launching speed. The size distribution of fragments is modeled with a power law fitted from observations of real asteroid surface. A full-scale demonstration is simulated using parameters specified by the mission. We report the results of the simulation, which include the computed spread of the ejecta cloud and the recorded history of ejecta accretion and escape. The violent period of the ejecta evolution is found to be short, and is followed by a stage where the remaining ejecta is gradually cleared. Solar radiation pressure proves to be efficient in cleaning dust-size ejecta, and the simulation results after two weeks shows that large debris on polar orbits (perpendicular to the binary orbital plane) has a survival advantage over smaller ejecta and ejecta that keeps to low latitudes.