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Development of Landing Experiment System using Rocket Sled

Authors :
EGUCHI, Hikaru
OKANO, Hiro
SHIBATA, Takuma
NAKATA, Daisuke
Source :
令和4年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium FY2022.
Publication Year :
2023
Publisher :
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS), 2023.

Abstract

令和4年度宇宙輸送シンポジウム(2023年1月12日-13日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)) , 相模原市, 神奈川県<br />Space Transportation Symposium FY2022 (January 12-13, 2023. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan<br />The flight demonstration of reusable rockets requires landing technologies such as deceleration and descent by engine throttling and shock absorption by landing legs. To achieve these landing technologies, this study aims to create a landing and descent environment using a rocket sled for reusable rockets. In this paper, we describe the landing and descent environment that can be achieved with the proposed experimental system, and also describe its current development status.<br />資料番号: SA6000184018<br />STCP-2022-018

Subjects

Subjects :
Landing
Reusable Rocket
Rocket Sled

Details

Language :
Japanese
Database :
OpenAIRE
Journal :
令和4年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium FY2022
Accession number :
edsair.jairo.........49d351be8e95f4d4062b6f21727b1af7