کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
1715133 1519966 2013 10 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Small carry-on impactor of Hayabusa2 mission
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
پیش نمایش صفحه اول مقاله
Small carry-on impactor of Hayabusa2 mission
چکیده انگلیسی

A Japanese spacecraft, Hayabusa2, the successor of Hayabusa, which came back from the Asteroid Itokawa with sample materials after its 7-year-interplanetary journeys, is a current mission of Japan Aerospace Exploration Agency (JAXA) and scheduled to be launched in 2014. Although its design basically follows Hayabusa, some new components are planned to be equipped in Hayabusa2 mission. A Small Carry-on Impactor (SCI), a small explosive device, is one of the challenges that were not seen with Hayabusa. An important scientific objective of Hayabusa2 is to investigate chemical and physical properties of the internal materials and structures. SCI creates an artificial crater on the surface of the asteroid and the mother spacecraft observes the crater and tries to get sample materials. High kinetic energy is required to creating a meaningful crater. The SCI would become complicated and heavy if the traditional acceleration devices like thrusters and rocket motors are used to hit the asteroid because the acceleration distance is quite large and guidance system is necessary. In order to make the system simpler, a technology of special type of shaped charge is used for the acceleration of the impact head. By using this technology, it becomes possible to accelerate the impact head very quickly and to hit the asteroid without guidance system. However, the impact operation should be complicated because SCI uses powerful explosive and it scatters high speed debris at the detonation. This paper presents the overview of our new small carry-on impact system and the impact operation of Hayabusa2 mission.


► Next asteroid exploration project HAYABUSA2 started supposing a launch in 2014.
► A small carry-on impactor (SCI) is one of the new challenges that were not seen with HAYABUSA.
► Technology of the special type of shaped charge is applied to new impact system.
► This paper describes the overview of the small carry-on impactor system and the result of the development test.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Acta Astronautica - Volume 84, March–April 2013, Pages 227–236
نویسندگان
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