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Functional Verification of Engineering Model of Non-explosive Shockless Holding and Release Mechanism Using Heating Wire Cutting Method

열선 절단 방식을 적용한 비폭발식 무충격 구속분리장치 EM의 기능검증

  • Oh, Hyun-Ung (Department of Aerospace Engineering, Chosun University) ;
  • Jeon, Su-Hyeon (Department of Aerospace Engineering, Chosun University)
  • Received : 2013.01.07
  • Accepted : 2013.04.18
  • Published : 2013.05.20

Abstract

Non-explosive shockless holding and release mechanism for a nano class small satellite application has been proposed and investigated. The great advantages of the mechanism are a much lower shock level and larger constraint force than the conventional mechanism using pyro and the heating wire cutting mechanism which has been generally applied to the cube satellite program. To investigate the effectiveness of the mechanism design, EM mechanism was developed and tested to verify the basic function of the mechanism. The test results indicate that the proposed mechanism is well functioning as the mechanism design intends.

Keywords

References

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Cited by

  1. Thermal Vacuum Test and Thermal Analysis for a Qualification Model of Cube-satellite STEP Cube Lab. vol.44, pp.2, 2016, https://doi.org/10.5139/JKSAS.2016.44.2.156