Cansat suborbital launch experiment-university educational space program using can sized pico-satellite

Our laboratory is proceeding with a project to design and fabricate a nano satellite named “Gekkabijin” as “CanSat” project. This project was agreed at USSS'98 as a Japan-U.S. joint venture to make satellites for educational purpose. CanSat is, as can be imaged from the name, a Coke can shaped...

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Published inActa astronautica Vol. 48; no. 5; pp. 767 - 776
Main Authors Sako, Nobutada, Tsuda, Yuichi, Ota, Shuichiro, Eishima, Takashi, Yamamoto, Toru, Ikeda, Ichirou, Ii, Hiromitsu, Yamamoto, Hidenori, Tanaka, Hideyuki, Tanaka, Akira, Nakasuka, Shinichi
Format Journal Article
LanguageEnglish
Published Elsevier Ltd 2001
Subjects
Education
Orbits
Rockets
Space research
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Abstract Our laboratory is proceeding with a project to design and fabricate a nano satellite named “Gekkabijin” as “CanSat” project. This project was agreed at USSS'98 as a Japan-U.S. joint venture to make satellites for educational purpose. CanSat is, as can be imaged from the name, a Coke can shaped and sized satellite. Our CanSat “Gekkabijin” was designed to deploy a thin flexible membrane using centrifugal force. Before we can launch a CanSat into space, we had a chance to put it into sub-orbit with a support from a U.S. amateur rocket group in the name of ARLISS Project. ARLISS Project has already taken place twice in 1999 and 2000 and we carried out 6 missions. This paper describes the objectives, satellite design, experiment results and lessons learned of University of Tokyo CanSat Project.
AbstractList Our laboratory is proceeding with a project to design and fabricate a nano satellite named "Gekkabijin" as "CanSat" project. This project was agreed at USSS'98 as a Japan-U.S. joint venture to make satellites for educational purpose. CanSat is, as can be imaged from the name, a Coke can shaped and sized satellite. Our CanSat "Gekkabijin" was designed to deploy a thin flexible membrane using centrifugal force. Before we can launch a CanSat into space, we had a chance to put it into sub-orbit with a support from a U.S. amateur rocket, group in the name of ARLISS Project. ARLISS Project has already taken place twice in 1999 and 2000 and we carried out 6 missions. This paper describes the objectives, satellite design, experiment results and lessons learned of University of Tokyo CanSat Project. copyright 2001 International Astronautical Federation. Published by Elsevier Science Ltd.
Our laboratory is proceeding with a project to design and fabricate a nano satellite named “Gekkabijin” as “CanSat” project. This project was agreed at USSS'98 as a Japan-U.S. joint venture to make satellites for educational purpose. CanSat is, as can be imaged from the name, a Coke can shaped and sized satellite. Our CanSat “Gekkabijin” was designed to deploy a thin flexible membrane using centrifugal force. Before we can launch a CanSat into space, we had a chance to put it into sub-orbit with a support from a U.S. amateur rocket group in the name of ARLISS Project. ARLISS Project has already taken place twice in 1999 and 2000 and we carried out 6 missions. This paper describes the objectives, satellite design, experiment results and lessons learned of University of Tokyo CanSat Project.
Author Tanaka, Hideyuki
Eishima, Takashi
Sako, Nobutada
Yamamoto, Toru
Tanaka, Akira
Nakasuka, Shinichi
Tsuda, Yuichi
Ikeda, Ichirou
Yamamoto, Hidenori
Ota, Shuichiro
Ii, Hiromitsu
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  givenname: Yuichi
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  email: cansat@space.t.u-tokyo.ac.jp
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References Sako, Tsuda, Ota, Eishima, Yamamoto, Ikeda, Ii, Yamamoto, Tanaka, Tanaka, Nakasuka (BIB5) 1999
Motohashi, Nakasuka (BIB3) 1998
Narusawa, Aoki, Nakasuka, Motohashi, Nagashima, Kawakatsu, Kinoshita (BIB2) 1998
Motohashi, Nakasuka, Aoki, Narusawa, Nagashima, Kawakatsu, Kinoshita (BIB1) 1998
University of Tokyo CanSat Webpage: http://www.space.t.u-tokyo.ac.jp/cansat
Nakasuka, Tsuda, Sako, Ota, Eishima, Yamamoto, Ikeda, Ii, Tanaka, Yamamoto (BIB4) 1999; 2
ARLISS Webpage: http://ssdl.stanford.edu/arliss
Narusawa (10.1016/S0094-5765(01)00039-X_BIB2) 1998
10.1016/S0094-5765(01)00039-X_BIB6
10.1016/S0094-5765(01)00039-X_BIB7
Motohashi (10.1016/S0094-5765(01)00039-X_BIB1) 1998
Nakasuka (10.1016/S0094-5765(01)00039-X_BIB4) 1999; 2
Motohashi (10.1016/S0094-5765(01)00039-X_BIB3) 1998
Sako (10.1016/S0094-5765(01)00039-X_BIB5) 1999
References_xml – year: 1999
  ident: BIB5
  article-title: CanSat-Basic Experiment of Solar Cell Attached Membrane Deployment
  publication-title: The 43rd Space Science and Technology Union Conference
  contributor:
    fullname: Nakasuka
– year: 1998
  ident: BIB2
  article-title: Behavior of Membrane Structure under Microgravity Environment
  publication-title: Proceedings of 21st ISTS, 98-b-16
  contributor:
    fullname: Kinoshita
– volume: 2
  start-page: 356
  year: 1999
  end-page: 359
  ident: BIB4
  article-title: University of Tokyo's participation in CanSat Project -A very small satellite project for educational purpose
  publication-title: Proceedings of the 2nd International Conference on Integrated MicroNanotechnology for Space Applications
  contributor:
    fullname: Yamamoto
– start-page: 146
  year: 1998
  end-page: 151
  ident: BIB3
  article-title: On-orbit Dynamics and Control of Large Scaled Membrane with Satellites at its Corners
  publication-title: Proceedings of IFAC Symposium on Aerospace Control
  contributor:
    fullname: Nakasuka
– year: 1998
  ident: BIB1
  article-title: On-orbit Dynamics and New Control Scheme for Large Membrane “Furoshiki” Satellite
  publication-title: Proceedings of 21st ISTS, 98-e-20
  contributor:
    fullname: Kinoshita
– start-page: 146
  year: 1998
  ident: 10.1016/S0094-5765(01)00039-X_BIB3
  article-title: On-orbit Dynamics and Control of Large Scaled Membrane with Satellites at its Corners
  publication-title: Proceedings of IFAC Symposium on Aerospace Control
  contributor:
    fullname: Motohashi
– volume: 2
  start-page: 356
  year: 1999
  ident: 10.1016/S0094-5765(01)00039-X_BIB4
  article-title: University of Tokyo's participation in CanSat Project -A very small satellite project for educational purpose
  publication-title: Proceedings of the 2nd International Conference on Integrated MicroNanotechnology for Space Applications
  contributor:
    fullname: Nakasuka
– year: 1998
  ident: 10.1016/S0094-5765(01)00039-X_BIB1
  article-title: On-orbit Dynamics and New Control Scheme for Large Membrane “Furoshiki” Satellite
  publication-title: Proceedings of 21st ISTS, 98-e-20
  contributor:
    fullname: Motohashi
– ident: 10.1016/S0094-5765(01)00039-X_BIB7
– year: 1998
  ident: 10.1016/S0094-5765(01)00039-X_BIB2
  article-title: Behavior of Membrane Structure under Microgravity Environment
  publication-title: Proceedings of 21st ISTS, 98-b-16
  contributor:
    fullname: Narusawa
– ident: 10.1016/S0094-5765(01)00039-X_BIB6
– year: 1999
  ident: 10.1016/S0094-5765(01)00039-X_BIB5
  article-title: CanSat-Basic Experiment of Solar Cell Attached Membrane Deployment
  publication-title: The 43rd Space Science and Technology Union Conference
  contributor:
    fullname: Sako
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Snippet Our laboratory is proceeding with a project to design and fabricate a nano satellite named “Gekkabijin” as “CanSat” project. This project was agreed at USSS'98...
Our laboratory is proceeding with a project to design and fabricate a nano satellite named "Gekkabijin" as "CanSat" project. This project was agreed at USSS'98...
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SubjectTerms Education
Orbits
Rockets
Space research
Title Cansat suborbital launch experiment-university educational space program using can sized pico-satellite
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