• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.46 no.3
• /
• pp.230-236
• /
• 2018

This paper deals with the improvement of pressurized quality for high maneuver aircraft. Anti-G Valve is a pressure regulating valve for inflating anti-G suits and providing a sense line signal for a g-compensated oxygen regulator. The new anti-g valve system is satisfied with military specification MIL-V-87255 and allowed the pilots to tolerate high-G exposures without any vibrations. The flight test was performed by two T/FA-50 pilots and other tests used the centrifuge made by anti-g developer. A comparison of the new anti-g valve with period one, it have better response and low chattering phenomenon.

• Journal of the military operations research society of Korea
• /
• v.34 no.3
• /
• pp.31-40
• /
• 2008

The aircraft manufacturing industry is a profitable business and has the potential to be an important export business. Our trade deficit needs to be improved in aircraft manufacturing part. Our national aircraft industry, which has been recognized for its quality in many domestic and international Air Shows, has developed the T/A-50 aircraft from the origins of the KT-1. With the ongoing development of the next generation fighter planes and helicopters, business for the next generation domestic air cargo has bright prospects. Judging by the history of the overseas air force dispatch during the Vietnam, Gulf, and Iraqi wars whose main mission was air transportation, there will be many opportunities to show the excellence of Korean air cargo in the future. The purpose of this study is to discover the optimal scale of air cargo development using the AHP method. The authors evaluated the scale of air cargo in size and capacity based on the following 5 standards used Korean developing airliner: usability, economics, technology, safety, and environmental friendliness. Then, the authors modified specific standards suitable for air cargo based on literature review Decision-making groups were chosen for suitability of expert staff in charge because they could represent for leading opinions in this specialized area especially as in practical aspects. The participants of the evaluation were pilots, transportation officers and management staff in the KAI who have experienced over 5years.

• Defense and Technology
• /
• no.5 s.255
• /
• pp.18-25
• /
• 2000

T-50은 제 3세대 훈련기의 특징을 최대한 살려서 Total Traing System으로서의 가치를 높여야 한다. 즉, 항공기 뿐만 아니라 비행시뮬레이터를 비롯한 각종 지상비행훈련장비와 정비훈련장비 등으로 Total Traing System으로서의 시너지 효과를 높이는데 주력해야 할 것이다. 또한 KT-1과 조화롭게 연계된 비행훈련체계를 구축함으로써 세계 훈련기시장에서 제 3세대 훈련기의 선두주자로서의 인식과 함께 마케팅에도 상호보완효과를 유도해 낼 수 있을 것으로 예상된다. 이제 세계 훈련기 시장의 종주국으로 거듭나고 있는 한국의 항공산업은 때마침 구조조정에 의해 새로 탄생된 한국항공우주산업(주)의 출범과 맞물려 세계 항공업계의 주목을 받기 시작했다.

• Journal of Aerospace System Engineering
• /
• v.11 no.3
• /
• pp.31-38
• /
• 2017

As demand for best practices relative to flight test safety management operations and processes in the aviation industry grows, standards for such aspects of the industry in Korea should be examined. Therefore, in this paper, we conducted flight test operation processes and safety management program development studies based on documents related to flight tests of the Korean civil aviation KC-100, the military aircraft T-50, the FAA (Federal Aviation Administration), and CAAC (Civil Aviation Administration of China) for performance validation, test evaluation and safety certification for aircraft under development and remodeling. In addition, we introduced and analyzed best practices of the FTSC (Flight Test Safety Committee) applicable to aircraft flight test processes.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.33 no.2
• /
• pp.106-112
• /
• 2005

Modern versions of supersonic jet fighter aircraft have several different weapon loading configuration to support air-to-air combat and air-to-ground delivery of weapon modes. These various aircraft loading conditions could result in asymmetric configurations to the aircraft once delivered. These asymmetric configurations could result in decreased handling qualities for the pilot maneuvering, stability, control issues and aerodynamic performance of the aircraft. In order to eliminate or decrease these adverse impacts on the pilot's ability, development of T-50 flight control law attempts to control the aircraft in both longitudinal and lateral-directional axes. Especially, the design of the lateral-directional roll axis control laws, utilizing a simple roll rate feedback structure and gains such as F-16, is developed for the T-50 aircraft to meet the aircraft's design requirements. Consequently, it is found that the improved control law decreases the roll-off phenomenon in lateral axes during pitch maneuver.

• Journal of Aerospace System Engineering
• /
• v.1 no.3
• /
• pp.21-25
• /
• 2007

This is a study on the establishment of airworthiness certification system fitted for korean military aircraft acquisition and export. Based on the investigation of US civil & military airworthiness system and analysis of the real state of domestic military aircraft acquisition, this paper offers some ideas that can be helpful to establish laws and organizations to certify airworthiness. Particularly this paper suggests that the best way to build airworthiness certification laws/guidelines and technical criteria, the optimal organizational structure which is decentralized by dividing administrative certification authority and technical research center.

• The Journal of Aerospace Industry
• /
• s.67
• /
• pp.1-21
• /
• 2004

항공우주 소재는 전반적인 재료기술을 이끌어가는 선도 분야로서, 재로기술 수준의 지표가 되고 있다. 항공우주에서 소재는 비행체의 기술적 가능성을 제공하는 기반기술 중의 하나로서 기술 및 산업적 파급효과가 매우 크다. 이렇듯 세계 항공우주 선진국은 소재분야에 기술개발과 투자를 확대하고 있다. 소재업체는 항공우주관련 업체 중 가장 많은 분포를 가지고 있으면, 최근 완제기 업체들의 합병으로 인해 부품소재공급 업체들의 공급사슬 재정립이 활발히 진행 중이다. 따라서 본고에서는 항공우주 소재 기술의 중요성과 국내외 기술 및 시장 동향을 파악하고 국내 항공우주 소재산업의 문제점을 살펴보았다. KT-1, T-50 등 성공적인 국내 항공기의 개발을 바탕으로 세계적인 항공우주산업국가로 도약하려는 우리나라의 상황에서 소재기술의 발전을 위한 산업육성과 기술개발 전략 방안 등을 모색해 보았다.

• Current Industrial and Technological Trends in Aerospace
• /
• v.5 no.1
• /
• pp.15-24
• /
• 2007

항공용 소프트웨어의 개발 및 인증은 현재까지 국내에서는 거의 경험이 없는 분야이다. 물론 각종 무인기 등의 개발사업을 통해 항공용 소프트웨어를 개발하고 시험한 사례는 다수 있으나, 체계적으로 개발 및 시험된 경우는 흔치 않다. 특히 유인기 분야에서는 거의 전무하다고 할 수 있다. KFP, KT-1, T-50 등의 군 사업을 통하여, 국외에서 개발된 소프트웨어에 대한 유지보수 경험 및 인력과, 이를 위한 체계가 구축되어 있는 정도라 할 수 있다. 이러한 상황에서, 이제는 항공용 소프트웨어를 국내에서 개발하고 시험, 인증할 수 있는 능력의 확보가 요구되고 있으며, 이는 국내 항공산업이 항공기 독자개발 능력 확보를 위해서는 필수적인 핵심기술이다. 이러한 기술력 확보를 위하여, 현재 항공용 소프트웨어 개발과 관련한 세계적인 흐름 및 최신의 기술동향을 파악하는 것이 무엇보다 필요하다. 항공선진국에서 이미 적용하지 않는 규격, 기술, 개발방식을 그대로 따라하는 과정을 거친다면, 경쟁력 확보는 요원한 일이기 때문이다. 따라서 본 논문에서는 항공용 소프트웨어 인증을 위한 규격의 역사 및 종류와, 현재 주로 적용되고 있는 DO-178B에 대한 주요 내용 및 현안에 대하여 살펴보고, 소프트웨어 개발과 관련한 소프트웨어 툴, 모델기반 개발 방식 등 해외 선진업체 및 기관들의 최신 기술동향을 정리하였다.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
• /
• v.26 no.11
• /
• pp.992-998
• /
• 2015

In case of UHF Band Transceiver for Army Aircraft, it shall follow MIL-STD-461F Figure CE101-4 most key design points for this equipment were to minize the current consumption and frequency interference since it will be integrated on aircraft. However, after design, abnomal signal(over 100 dBuA) was occured from 30 Hz to 1 kHz on CE101 test. Occured abnomal signal was measured as 50 Hz signal which was tansceiver $T_{DD}$ signal with the output power of 10 W and 20 ms periods. To meet the specification, current variation needed to be minized. Thus, $I_{dq}$ and $I_d$ of power amplifier were modified almost equally through test result and finally, the equipment was designed and developed with no difference of current consumption and frequency interference from the previous design goal.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.32 no.6
• /
• pp.117-125
• /
• 2004

This paper describes the test technique for the full-scale airframe durability test according to the military handbook(MIL-HDBK-1530) and ASIP(Aircraft Structure Integrity Program) to evaluate structural integrity and to obtain basic data for IPA(Initial Production Approval) of the Korean advanced trainer(T-50). This paper covers the full-scale airframe floating setup technique, the optimized test load simulation method, test rig design technique, test setup design and installation techniques, test safety device design and operation technique, and durability test results. As 1st life durability test was successfully performed, it was confirmed that this method is available in a full-scale airframe structural test.