• Title/Summary/Keyword: 시험기관

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Impact Test and Evaluation for HTPE IM Rocket Motor (HTPE 둔감 추진기관의 충격 시험 및 평가)

  • Kim, Chang-Kee;Lee, Do-Hyung;Yeon, Jeong-Mo;Yoo, Ji-Chang
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.163-166
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    • 2009
  • Bullet and fragment impact test with rocket motors was performed and characteristics of the results were analyzed. The material of the motor case was carbon epoxy composite. The motor was loaded with HTPE propellants to improve the insensitive munitions characteristics. In the tests, sound pressure and heat flux sensors were used to determine the category of response according to the standard. The reaction response of all of the HTPE motors impacted by bullet and fragment was judged as Type V burning.

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The implementation of the firing control system considering a flight sequence control technique (비행시퀀스제어기법을 적용한 점화통제시스템 구현)

  • Lee, Seung-Jae
    • Journal of the Korean Society of Propulsion Engineers
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    • v.12 no.3
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    • pp.41-48
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    • 2008
  • One of main functions of the firing control system applied to a rocket propulsion test has been to provide electric current for ignition of a solid rocket motor. This paper describes the design and implementation of an enhanced firing control system for ground propulsion test that can also control and verify various types of squib events and flight sequences.

Hypersonic Engine Test Facility Operation Test : Ejector System Performance Analysis (고속추진기관 시험설비 시운전 : 이젝터시스템 성능분석)

  • Kang, Sang-Hun;Lee, Yang-Ji;Oh, Joong-Hwan;Yang, Soo-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.05a
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    • pp.268-271
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    • 2010
  • Hypersonic engine test facility with ejector system was tested. Ejector system was designed by revised EJSIMP code. The performance of the ejector system was predicted by numerical analysis. As a result, ejector system satisfied the facility design requirement. Based on the pressure level, the facility was successfully started at Mach 3.5 and 20km altitude condition.

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선박성능과 기관성능의 예측 프로그램

  • 안시영
    • Bulletin of the Society of Naval Architects of Korea
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    • v.31 no.4
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    • pp.22-25
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    • 1994
  • 선체성능, 선박운항성능 및 기관성능의 현황파악과 예측을 하는 것은 선박설계자, 선박운항자 및 선박관리운영자에게 설계, 보선관리 및 용역관리상 대단히 중요하다. 선체성능의 전산원용예측에 관한 대부분의 문헌은 모형수조시험 및 공시해상시험의 자료를 수식화하는 데 집중하고 있다. 따라서 현재까지 자료의 수식화, 예측된 자료와 성능시험결과치의 상관기법 및 PC soft ware를 이용한 선박성능예측의 체계적 접근법 등에 관한 연구가 활발히 진행되어 왔다. 또한 선박의 Abstract Log Book의 자료 및 주기관 성능자료의 수식화, PC soft ware 개발에 의한 선박운 항성능 및 기관성능예측에 대한 연구가 역시 수행되고 있다. 이와 관련하여 본 고에서는 선체 성능(저항과 추진계수), 선박운항성능 및 주기관성능의 예측에 관하여 그 개요를 소개코져 한다.

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공지사항

  • Korea Electronics Association
    • Journal of Korean Electronics
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    • v.5 no.11
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    • pp.98-99
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    • 1985
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