3321 CAMUI型ハイブリッドロケットによるCanSat実験(S86-1 小型宇宙システム(1),S86 小型宇宙システム)

青柳 賢英; 佐藤 立博; 岩本 隆敏; 竹浪 恭平; 難波江 亮; 下岡 彩子; 佐鳥 新; 三橋 龍一; 大滝 誠一; 豊田 国昭; 永田 晴紀

doi:10.1299/jsmemecjo.2005.5.0_369

2005.5

Session ID : 3321

DOI https://doi.org/10.1299/jsmemecjo.2005.5.0_369

Conference information

3321 CanSat experiment by CAMUI Hybrid Rocket

Yoshihide Aoyanagi, Tatuhiro Sato, Takatoshi Iwamoto, [in Japanese], Akira Nabae, Ayako Simooka, Shin Satori, Ryuichi Mitsuhashi, Seiichi Ohtaki, Kuniaki Toyota, Harunori Nagata

Author information

Yoshihide Aoyanagi
Hokkaido Institute of Technology
Tatuhiro Sato
Hokkaido Institute of Technology
Takatoshi Iwamoto
Hokkaido Institute of Technology
[in Japanese]
Hokkaido Institute of Technology
Akira Nabae
Hokkaido Institute of Technology
Ayako Simooka
Hokkaido Institute of Technology
Shin Satori
Hokkaido Institute of Technology
Ryuichi Mitsuhashi
Hokkaido Institute of Technology
Seiichi Ohtaki
Hokkaido Institute of Technology
Kuniaki Toyota
Hokkaido Institute of Technology
Harunori Nagata
Hokkaido University

Keywords: Space development, Micro satellite, CanSat, Hokkaido Satellite

CONFERENCE PROCEEDINGS RESTRICTED ACCESS

Details

Abstract

The CanSat project was conducted by undergraduate students who had designed and fabricated a small experimented module called "CanSat". The CanSat was launched by a CAMUI-type hybrid rocket up to the height of 330meters. The CanSat was ejected from the rocket by the releasing mechanism that was installed inside the fairing of rocket, and fell down safely by using a parachute.

Corresponding author

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