Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
University of Tokyo Graduate School
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
出版者
宇宙航空研究開発機構宇宙科学研究本部
出版者（英）
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
雑誌名
第15回アストロダイナミクスシンポジウム講演後刷り集 2005
雑誌名(英)
Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics
Reported in this paper is the result of the mission analysis of asteroid flyby missions using miniature asteroid interceptors. Two types of mission concept are considered. The first is a mission concept with an interceptor boosted from GTO (Geostationary Transfer Orbit) by small solid rocket motor (assuming the piggy back launch of geostationary satellite). The second is a mission concept with four interceptors loaded on a mother carrier spacecraft, launched together and released on orbit to target four different asteroids. The results of the trajectory analysis and operation sequence investigation are reported in the paper.
Mission analysis of asteroid flyby exploration by miniature asteroid interceptors
