2021年
Separation Experiment for OMOTENASHI Moon Lander at Extremely High Spin Rates
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
- 巻
- 19
- 号
- 4
- 開始ページ
- 453
- 終了ページ
- 460
- 記述言語
- 英語
- 掲載種別
- DOI
- 10.2322/tastj.19.453
- 出版者・発行元
- 一般社団法人 日本航空宇宙学会
<p>This paper describes a separation experiment conducted at extremely high spin rates for OMOTENASHI, being developed as the world's smallest Moon lander. The experiment validated the separation method used in the landing sequence and the tipoff impulse was estimated from the motion of the separated object. The study showed that the tipoff impulse increases superlinearly in the high spin rate region. This information is indispensable in determining the operational spin rate of OMOTENASHI in orbit. The method described in this paper can be applied widely to separation experiments for small spinning satellites and rocket stages.</p>
- リンク情報
- ID情報
-
- DOI : 10.2322/tastj.19.453
- CiNii Articles ID : 130008062309