| Item type |
会議発表論文 / Conference Paper(1) |
| 公開日 |
2023-05-23 |
| タイトル |
|
|
タイトル |
1J/1W-PPTシステム搭載1Uキューブサット・大阪産業大学OSU-1号機の開発とOSU-2,3,4,5号機の構想 |
| 言語 |
|
|
言語 |
jpn |
| 資源タイプ |
|
|
資源タイプ識別子 |
http://purl.org/coar/resource_type/c_5794 |
|
資源タイプ |
conference paper |
| その他のタイトル（英） |
|
|
その他のタイトル |
Development of Osaka Sangyo University 1U Cubesat OSU-1 with 1J/1W Pulsed Plasma Thruster Systems, and Plans of Nano-Satellites and Probes OSU-2, 3, 4 and 5 |
| 著者 |
岡, 廉一朗
平田, 稜
郷, 隼人
池内, 圭輝
木村, 友則
九里, 孝行
田原, 弘一
池田, 知行
脇園, 堯
OKA, Ren-ichiro
HIRATA, Ryo
GO, Hayato
IKEUCHI, Yoshiki
KIMURA, Tomonori
KURI, Takayuki
TAHARA, Hirokazu
IKEDA, Tomoyuki
WAKIZONO, Takashi
|
| 著者所属 |
|
|
|
OSU太陽系宇宙開発プロジェクト |
| 著者所属 |
|
|
|
OSU太陽系宇宙開発プロジェクト |
| 著者所属 |
|
|
|
大阪産業大学 |
| 著者所属 |
|
|
|
大阪産業大学 |
| 著者所属 |
|
|
|
OSU太陽系宇宙開発プロジェクト |
| 著者所属 |
|
|
|
OSU太陽系宇宙開発プロジェクト |
| 著者所属 |
|
|
|
大阪産業大学 |
| 著者所属 |
|
|
|
東海大学 |
| 著者所属 |
|
|
|
ハイサーブ |
| 著者所属（英） |
|
|
|
en |
|
|
OSU Solar System Space Development Project |
| 著者所属（英） |
|
|
|
en |
|
|
OSU Solar System Space Development Project |
| 著者所属（英） |
|
|
|
en |
|
|
Osaka Sangyo University |
| 著者所属（英） |
|
|
|
en |
|
|
Osaka Sangyo University |
| 著者所属（英） |
|
|
|
en |
|
|
OSU Solar System Space Development Project |
| 著者所属（英） |
|
|
|
en |
|
|
OSU Solar System Space Development Project |
| 著者所属（英） |
|
|
|
en |
|
|
Osaka Sangyo University |
| 著者所属（英） |
|
|
|
en |
|
|
Tokai University |
| 著者所属（英） |
|
|
|
en |
|
|
High-Serve |
| 出版者 |
|
|
出版者 |
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) |
| 出版者（英） |
|
|
出版者 |
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS) |
| 書誌情報 |
令和4年度宇宙輸送シンポジウム: 講演集録
en : Proceedings of Space Transportation Symposium FY2022
発行日 2023-01
|
| 会議概要（会議名, 開催地, 会期, 主催者等） |
|
|
内容記述タイプ |
Other |
|
内容記述 |
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 |
| 会議概要（会議名, 開催地, 会期, 主催者等）（英） |
|
|
内容記述タイプ |
Other |
|
内容記述 |
Space Transportation Symposium FY2022 (January 12-13, 2023. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan |
| 抄録（英） |
|
|
内容記述タイプ |
Other |
|
内容記述 |
In April 2020, Professor Tahara's group started a new nano-satellite/probe R&D project in Osaka Sangyo University (OSU) after the Project of OIT Electric-Rocket-Engine onboard Small Space Ship (PROITERES) was terminated. In the 1st PROITERES, a nano-satellite with an electrothermal pulsed plasma thruster (PPT) was launched by Indian PSLV C-21 rocket on September 9th in 2012. The main mission was to accurately measure thrust performance in space and to change orbital altitude with the PPT. Currently, the OSU-2 nano-satellite (modified PROITERES-2 satellite) is being developed in OSU for launching in 2024 or 2025. The mission is a long-distance powered flight 50-100 km in altitude by high-power electrothermal PPTs. If altitude control is successful, possibility of small/nano-satellites will be widened. In order to achieve the powered flight, a long-time PPT operation is needed for the system of the OSU-2 satellite. Therefore, a new PPT system with a Multi Discharge Room (MDR), called MDR-PPT, was developed and successfully operated. The weight of the OSU-2 satellite is 47 kg; the outside dimension is 470 x 470 x 450 mm, and the electric power is 60 W. The OSU-2 satellite mainly consists of five systems of thruster system, structure system, attitude control system, communication system and C & DH system. All systems were developed with technologies of 1st PROITERES R&D. The OSU-1 nano-satellite, cubesat 1U (1kg), which is provided with a very-low-power PPT system for orbital transfer and attitude control, is also being developed for launching in 2024-2025. Furthermore, the OSU-3 probe is under development for lunar exploration by Hall thruster. The 4th OSU satellite is planned as a nano-satellite to achieve a main mission that space debris makes deorbit by electric propulsion. The principle of deorbiting space debris is exposure of plasma flow exhausted from an electric thruster to space debris; that is, reaction impulse from the flow is given to debris, and after that debris decreases velocity and deorbits. Accordingly, the OSU-4 satellite can deorbit space debris with safety without contacting to space debris and the satellite. Now, the OSU-4 satellite is under development for launching in 2024-2026. |
| 著者版フラグ |
|
|
出版タイプ |
AM |
|
出版タイプResource |
http://purl.org/coar/version/c_ab4af688f83e57aa |
| 資料番号 |
|
|
内容記述タイプ |
Other |
|
内容記述 |
資料番号: SA6000184060 |
| レポート番号 |
|
|
内容記述タイプ |
Other |
|
内容記述 |
STEP-2022-008 |
SA6000184060.pdf (1.3 MB)
