• 시스템엔지니어링워크숍
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• s.6
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• pp.86-93
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• 2005

본 논문은 KT-1 수출용 항공기(XKT-1,이하 XKT-1이라 함) 조종실배열 요소에 대한 정성적 ,정량적 반영 사항을 기술한 것으로,KT-1 동급항공기 조종실의 전형적 배열, 최신 항공기 현황과 더불어 조종실배열의 향후 추세에 관하여 고찰하였으며, 이를 바탕으로 여러 국가들의 요구사항 및 추세에 맞는 XKT-1 조종실배열의 특징과 설계결과를 나타내었다. XKT-1의 조종실배열은 잠재 고객이 선호하는 계기 및 시현기 등이 Human Engineering에 의거 최적의 배열이 되었으며 무엇보다 경쟁기종 대비 전방시야가 우수한 것으로 판명되었다.

• Journal of the Korean Society of Systems Engineering
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• v.17 no.1
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• pp.97-106
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• 2021

The purpose of the study on the tailoring of environmental requirements for KT-1 Export Version(XKT-1T) aircraft is not only based on meeting the compliance of the environmental reliability, customer satisfaction, but also for the expansion of its export. This paper proposes the environmental requirements tailoring processes and High/Low temperature conditions, test procedures, and the results of test profiles for the aircraft. Amongst many existing environmental requirements, the temperature requirements are considered as the most basic and the most important environmental requirements. The High/Low temperature tests are considered and tailored to the high and low temperature methods of MIL-STD-810.

• Journal of Aerospace System Engineering
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• v.15 no.3
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• pp.105-113
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• 2021

This paper delineates the applied thermal environmental test profiles using test conditions and procedures based on MIL-STD-810 Method 501 (High Temperature Test Method) and Method 502 (Low Temperature Test Method). The test profiles have been optimized in order to comply with export customer's requirements and product reliability in high and low temperature environment for XKT-1 (KT-1 Export Version) aircraft. Additionally, the tests are suitable for large sized environmental chambers, which is one of the facilities of ADD (Agency for Defense Development) according to ETEMP (Environmental Test and Evaluation Master Plan). The results of these test profiles and test executions satisfy the customer requirements and product reliability. The present paper can be applied to the other export programs with more severe temperature conditions.

• 한국항공운항학회:학술대회논문집
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• 2007.12a
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• pp.72-75
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• 2007

• Aerospace Industry
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• s.90
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• pp.54-56
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• 2006

한국항공우주산업(주) 벨사에 헬기 동체 1억5000만 달러 수출/대한항공,다목적실용위성 설계/산자부,항공우주부품기술개발에 115억 원 지원/KAI, XKT-1 총조 립 착수/대한항공,주한 미군RC-12 기체 창정비 1호기 인도/다목적실용위성2호,7월발사/F-15K,SLAM-ER 미사일 발사 성공/P-3C 2차 사업 성능개량 착수/ 대한항공 안전평가 세계 12위/한국 우주인 본격 추진

• Journal of the Korean Society for Aviation and Aeronautics
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• v.16 no.4
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• pp.20-25
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• 2008

The purpose of this study is leading to reduce the setup time and cost of the ground telemetry system for FA-50 program. And using the accumulated experience during T-50 and TA-50 development period, remove the risk of development and construct the optimal ground telemetry system for FA-50. For this study, collect the ground telemetry data of the T-50/TA-50, analyze the data and problems and then suggest the optimal telemetry ground system for FA-50.