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Hayabusa2's kinetic impact experiment: Operational planning and results

Authors :
Kent Yoshikawa
Hirotaka Sawada
Takanao Saiki
Seiji Sugita
Yuichi Tsuda
Satoru Nakazawa
Fuyuto Terui
Yuya Mimasu
Yuto Takei
Sei-ichiro Watanabe
Masahiko Arakawa
Makoto Yoshikawa
Naoko Ogawa
Go Ono
Source :
Acta Astronautica. 175:362-374
Publication Year :
2020
Publisher :
Elsevier BV, 2020.

Abstract

Hayabusa2 is a Japanese interplanetary probe launched on December 3, 2014, which arrived at asteroid Ryugu on June 27, 2018. During its stay around Ryugu, it completed several challenging operations, including deploying two rovers and a lander, conducting two sample collections, and performing a kinetic impact experiment. The kinetic impact experiment was one of the biggest challenges of the Hayabusa2 mission. Investigating the physical and chemical properties of asteroid internal materials and structures is an important scientific objective for small body exploration. We developed a small kinetic impactor called the SCI (Small Carry-on Impactor) to achieve this objective. The SCI is a compact kinetic impactor designed to remove a small region of Ryugu's uppermost surface regolith layer and create an artificial crater. The spacecraft deployed the SCI on April 5, 2019, successfully creating an artificial crater with a diameter of 15 m. This paper describes the operational planning of the kinetic impact experiment and summarizes the operation results.

Details

ISSN :
00945765
Volume :
175
Database :
OpenAIRE
Journal :
Acta Astronautica
Accession number :
edsair.doi...........41a86053cd175f2407396be5079764b0