The Development of a Satellite Ejection System of PRISM

  • KUSAKAWA Y
  • CHIKURA S
  • SHIMIZU K
  • et al.
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Abstract

Intelligent Space Systems Laboratory (ISSL) developed two CubeSats and develops the nano-scale remote-sensing satellite, "PRISM." Two CubeSats are now in orbit and PRISM is now preparing for a launch. PRISM is so small that it has no rocket interface with it and another structure, "PHS," which stands for PRISM Housyutu Souchi, plays a role of it. At the time of launches of two CubeSats ISSL developed an ejection system, T-POD and it succeeded separating four CubeSats. The authors consider that T-POD has high reliability enough and the authors develop PHS as an improved version of T-POD. In addition PHS has some original mechanism and structure, the reliability keeping mechanism, the flexible boom-defending mechanism and the putting in turnstile antenna structure.

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APA

KUSAKAWA, Y., CHIKURA, S., SHIMIZU, K., KOMATSU, M., & NAKASUKA, S. (2009). The Development of a Satellite Ejection System of PRISM. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN, 7(ists26), Tc_13-Tc_17. https://doi.org/10.2322/tstj.7.tc_13

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