• Title/Summary/Keyword: Electro-Mechanical Ignition Safety Device

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Development of Electro-Mechanical Ignition Safety Device (전기-기계식 점화안전장치 개발)

  • Jang, Seung-Gyo;Kang, Ho-Joon
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.332-335
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    • 2011
  • Electro-Mechanical Ignition Safety Device(EMISD) for solid rocket motor is designed and manufactured. The EMISD utilizes a true rotary solenoid for arming mechanism and an electric squib(initiator) for generating ignition energy. In order to prove the ignition capability of the EMISD, 10-cc Closed Bomb Test(CBT) is performed, which measures the pressure built by high temperature and high pressure gas generated by operating EMISD.

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Design and Output Characteristic Analysis of Electro-Mechanical Ignition Safety Device (전기-기계식 점화안전장치 설계 및 출력 특성 해석)

  • Jang, Seung-Gyo;Lee, Hyo-Nam;Oh, Jong-Yun;Oh, Seok-Jin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.39 no.12
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    • pp.1166-1173
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    • 2011
  • Electro-Mechanical Ignition Safety Device(EMISD) for solid rocket motor is designed and manufactured. The EMISD utilizes a true rotary solenoid for arming mechanism and an electric squib(initiator) for generating ignition energy. In order to prove the ignition capability of the EMISD, 10-cc Closed Bomb Test(CBT) is performed, which measures the pressure built by high temperature and high pressure gas generated by operating EMISD. The pressure built in the free volume of 10-cc closed bomb and the opening time of the ignition gas outlet are calculated using one dimensional gas dynamic model which is composed of the ideal gas equation and mass-energy conservation equation. Comparing the test result with model prediction, it is realized that the pressure built in the free volume of closed bomb due to the firing of EMISD, has the efficiency ratio of about 34%.

Development of Arm Fire Device for Solid Rocket (고체 추진기관 점화안전장치 개발)

  • Jang Seung-Gyo;Jung Jin-Suk;Kim In-Suk
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2005.11a
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    • pp.169-172
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    • 2005
  • The performance test result of the Arm Fire Device(Ignition Safety Device) for solid rocket which prevents accidental ignition was described. The results of the closed bomb test and the igniter test of the classical mechanical arm fire device and the advanced electro-mechanical arm fire device were presented, and according to the igniter test result it was realized that the electro-mechanical arm fire device has an advantage in aspect of the action time.

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