• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2015.10a
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• pp.567-569
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• 2015

To response quickly rapidly changing threats, and to reduce development and operational maintenance budget, U.S. Navy has been significantly applied commercial communication equipments instead of MIL-SPEC equipments. Starting from Aegis Baseline 7 combat system, components of systems were replaced to COTS-based system, and Littoral Combat Ships(LCS) and Zumwalt class destroyers have fully COTS-based combat system. In this paper, it is surveyed and analyzed that cases of COTS-based systems were applied and is compared difference from each type of ships.

• Journal of Korean Society for Quality Management
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• v.46 no.3
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• pp.379-396
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• 2018

Purpose: The purpose of this study was to propose a standard form of noise filter drawing, which is widely used in the field of weapon systems, to define the essential specification which is not standardized at the existing drawings and to employ the reference for manufacturing and qualification test. Methods: To do that, it identifies the improvements to analyze 19 noise filter drawings, studies the principle of noise filtering to find the essential part of the spec. and reviews the MIL-STD-220C and KS IEC 60939, which is the widely used as a formal spec. pertaining to the noise filter. Throughout the study, a standard form is developed to standardize the attenuation characteristics and find eight crucial metrics to specify the noise filter. Results: The results of this study are as follows; The standardized drawings can be used as the qualification test of the item and the manufacturing and engineering documents to make the noise filter, which are also applicable to the reference document to review KDS(Korea Defense Standard) drawings.

• Proceedings of the KSR Conference
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• 1998.05a
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• pp.194-202
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• 1998

This paper shows two models of the duplex system having a fault tolerant system characteristic used in airplane and railway system. The architecture of these systems is based on Mc68000, and we designed the single system, single duplex system, dual system and dual duplex system to evaluate the system characteristic. We calculate the failure rate of components using MIL-SPEC-2l7F and evaluate the reliability, avaliability, safety and MTTF(Mean Time To Failure) of the designed systems by Markov model. We choose our system depending on the developing system characteristic.

• Defense and Technology
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• no.4 s.218
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• pp.48-57
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• 1997

미 국방성에선 '94년 6월부터 PERRY 전 국방장관 지시에 의거 방위산업의 원가절감을 이유로 약 3만종의 군사규격중 30%에 해당하는 9천여종이 사용취소나 상용규격으로 바뀌는 대대적인 규격개혁 작업이 진행되었다. 이러한 변화는 미국과 군사규격체계를 공유하는 한국에도 직.간접으로 영향을 미칠것이라 판단되어, 변화를 인식하고 사전에 대비해야 할 필요성 때문에 이 글을 작성하게 되었다. 이 자료는 ‘94년 6월부터 '96년 6월까지 2년간 미 국방성에서 규격 개혁작업한 내용을 번역한 것으로 방위산업체와 규격관련 담당관의 검토가 필요하리라 판단된다.

• Journal of Aerospace System Engineering
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• v.8 no.2
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• pp.27-32
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• 2014

From the flight safety and the performance point of views, a new engine installation impacts an helicopter development or upgrade program significantly. More than a close relationship between an aircraft manufacturer and an engine manufacturer is necessary for the best integration work from the program initiation phase. In this paper, technical cooperation between aircraft and engine companies, and technical supports by the engine manufacturer for the T700/701K engine during the Surion development program are summarized. The applications of official technical program documents, US Mil-spec, France airworthiness regulations as the standard of the engine installation work, and engineering activities at each phase such as contract, design and manufacturing, flight clearance, ground and flight tests are described. This paper would be a cornerstone for the future domestic helicopter development program.

• Proceedings of the KIEE Conference
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• 1998.07a
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• pp.375-377
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• 1998

This paper shows two models of the TMR system- fail passive system - having a fault tolerant system characteristic used in airplane and railway system. We design the single system, single-voter TMR system and triplicated voter TMR system based on MC68000 and calculate the failure rate of components using MIL-SPEC-217F and evaluate the reliability and MTTF(Mean Time To Failure) of the designed systems by Markov model.

• Journal of the Korean Society for Aviation and Aeronautics
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• v.20 no.2
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• pp.7-12
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• 2012

A landing gear absorbs the impact energy during the touchdown and it generally consists of an oleo-pneumatic shock absorber and structural components. It should be designed not only to satisfy the static and fatigue strength requirements but to have the sufficient shock absorbing efficiency. The design loads and shock absorbing performance are to be validated by tests, which is required by MIL Spec and FAR, etc. This paper presents the development procedures from the design requirements to the qualification tests and technical points to be considered, with examples of the helicopter landing gear development.

• Proceedings of the ESK Conference
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• 1992.10a
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• pp.22-25
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• 1992

항공산업은 그 특성상 고도의 신뢰성, 안정성이 요구되며, 이를 충족시키기 위하여는 복잡하고 정밀한 구조를 가져야 하므로 다른 산업제품과는 비교가 안될 정도로 그부가가치를 가지고, 타 산업에의 기술 파급 효과가 역시 지대하다. 따라서, 우리나라와 같이 부존자원이 빈약하나 인적 자원이 우수하고 풍부한 나라에서는 자원절약형 산업인 항공산업의 타당성을 검토, 장기적인 육성방안을 수립하여 추진하는 것은 시대적인 요구라 할 수 있다. 이러한 요구에 따라 국방과학연구소에서 공군의 초, 중등훈련기 개발을 추진 중에 있음은 KFP(Korea Fighter Program)사업과 함께 매우 중요한 의미을 갖는다. 이와 같은 시점에서 한국인의 인체특성에 보다 적합한 항공기의 개발은 가장 시급한 과제이며, 이 문제점을 극복하기 위한 기본연구로 조종실 내부설계에 필요한 기준점 및 치수, MIL-SPEC에서 규정하고 있는 기준치를 분석하였으며 실제 항공기(F-5, F-4, F-16)칫수를 측정하여 이를 정면도, 측면도, 평면도로 제시하고, 항공기 제어계통인 조종간, 동력제어기, 러더페달 및 조종석의 실제 측정치와 공군 조종사의 인체측정치를 비교, 평가하였다. 또한 전투기들의 정면 계기판과 좌, 우측의 제어판의 표시장치 및 조작기들을 기능별로 구분하여 각 요소별 제한조건 및 설계지침들을 비교, 분석하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.38 no.11
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• pp.1130-1135
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• 2010

The main function of a landing gear is to absorb the impact energy during touchdown. Most landing gear use an oleo-pneumatic shock absorber which essentially consists of an oil damper and a gas spring. The performance of a shock absorber can be estimated by analysis but it should be verified by drop test, which is required by MIL Spec. and FAR. In the drop test, various data such as ground loads, shock absorber pressure, stroke and mass travel are analyzed to validate the shock absorbing efficiency and the mathematical model for analysis. This paper presents the introduction of drop test facility, the test procedure and data evaluation method with real drop test example.