Study on behavior of a spacecraft with membrane aeroshell in super low earth orbit and flight demonstration using a nanosatellite.
| Project/Area Number |
15H04205
|
|---|
| Research Category |
Grant-in-Aid for Scientific Research (B)
|
| Allocation Type | Single-year Grants |
|---|
| Section | 一般 |
|---|
| Research Field |
Aerospace engineering
|
|---|
| Research Institution | Japan Aerospace EXploration Agency |
|---|
Principal Investigator |
YAMADA Kazuhiko 国立研究開発法人宇宙航空研究開発機構, 宇宙科学研究所, 准教授 (20415904)
|
|---|
| Co-Investigator(Kenkyū-buntansha) |
永田 靖典 岡山大学, 自然科学研究科, 助教 (20635594)
高橋 裕介 北海道大学, 工学研究院, 助教 (40611132)
莊司 泰弘 大阪大学, 工学研究科, 助教 (70582774)
|
|---|
| Co-Investigator(Renkei-kenkyūsha) |
SUZUKI Kojiro 東京大学, 新領域創成科学研究科, 教授 (10226508)
IMAMURA Osamu 日本大学, 生産工学部, 准教授 (50436515)
AKITA Daisuke 東京工業大学, 理工学研究科, 准教授 (30435812)
ISHIMURA Kosei 宇宙航空研究開発機構, 宇宙科学研究所, 准教授 (10333626)
NAKASHINO Kyoichi 東海大学, 工学部, 准教授 (60408028)
|
|---|
| Project Period (FY) |
2015-04-01 – 2018-03-31
|
| Project Status |
Completed (Fiscal Year 2017)
|
| Budget Amount *help |
¥12,610,000 (Direct Cost: ¥9,700,000、Indirect Cost: ¥2,910,000)
Fiscal Year 2017: ¥2,210,000 (Direct Cost: ¥1,700,000、Indirect Cost: ¥510,000)
Fiscal Year 2016: ¥4,420,000 (Direct Cost: ¥3,400,000、Indirect Cost: ¥1,020,000)
Fiscal Year 2015: ¥5,980,000 (Direct Cost: ¥4,600,000、Indirect Cost: ¥1,380,000)
|
|---|
| Keywords | 超小型衛星 / 大気圏突入 / 柔軟構造体 / 希薄気体 / 展開構造物 / 航空宇宙工学 / 柔軟構造物 / 再突入機 / 柔軟構造 |
|---|
| Outline of Final Research Achievements |
In this study, the behavior of a spacecraft with low-mass and large membrane aeroshell in super low earth orbit is measured in real flight using the nanosatellite EGG. The group of attitude sensors including inertial sensor, optical sensor and faraday cup sensors which can be installed in nanosatellite EGG was developed. In EGG’s flight operation, we acquired a lot of valuable flight data related to attitude motion and orbit change of a spacecraft with a membrane aeroshell. For example, an orbit change history of EGG by the aerodynamic force acting on the membrane aeroshell in rarefied flow was observed continually. These flight data are expected to be useful for the development of an important technology for nano-satellite, that is, an orbit collapse technology to prevent from becoming space debris.
|
Report
(4 results)
Research Products
(30 results)
-
-
[Presentation] Re-entry Nano-Satellite with Gossamer Aeroshell and GPS/Iridium Deployed from ISS2017
Author(s)
Kazuhiko Yamada , Takahiro Moriyoshi , Kazushige Matsumaru , Hiroki Kanemaru , Takahiro Araya , Kojiro Suzuki , Osamu Imamura , Daisuke Akita , Yasunori Nagata , Yasuhiro Shoji , Yusuke Takahashi , Yasumasa Watanabe , Takashi Abe
Organizer
31st International Symposium on Space Technology and Science
Related Report
Int'l Joint Research
-
[Presentation] Flight experiment of nano-satellite "EGG" for deployment demonstration of membrane aeroshell2017
Author(s)
Kazuhiko Yamada, Takahiro Moriyoshi, Kazushige Matsumaru, Hiroki Kanemaru, Takahiro Araya, Kojiro Suzuki, Osamu Imamura, Daisuke Akita, Yasunori Nagata, Yasuhiro Shoji, Yusuke Takahashi, Yasumasa Watanabe, Takashi Abe
Organizer
14th International Planetray Probe Workshop
Related Report
Int'l Joint Research
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
