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http://dx.doi.org/10.5139/JKSAS.2007.35.10.948

Flight Test of Propulsion System for Verifying Engine/Aircraft Compatibility of T-50 Advanced Trainer  

Lee, Sang-Hyo (한국항공우주산업(주))
Jeong, In-Myon (한국항공우주산업(주))
Jung, Joo-Hyun (한국항공우주산업(주))
Shim, Jae-Kwang (한국항공우주산업(주))
Kang, Sung-Soo (한국항공우주산업(주))
Park, Sung-Hwan (한국항공우주산업(주))
Han, Byoung-Hak (한국항공우주산업(주))
Moon, Hyung-Rae (한국항공우주산업(주))
Cha, Jae-Byoung (한국항공우주산업(주))
Lee, Boo-ll (한국폴리텍 항공대학)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.35, no.10, 2007 , pp. 948-956 More about this Journal
Abstract
It is important during FSD(Full Scale Development) period to verify whether the aircraft system function meets the aircraft requirements and functional performance. Especially, the functionality of the integrated propulsion system should be verified to evaluate the compatibility with aircraft. Various flight tests such as the engine airstart test, the engine horsepower extraction test, the backup throttle functionality test had been performed to evaluate the engine/aircraft compatibility with T-50 during FSD period. Through such flight tests, it was confirmed that the propulsion system of T-50 was properly designed and installed to the aircraft. This paper shows description on each flight test item, test procedure and test results. It is expected that this paper could be a reference for preparing the propulsion flight test in other aircraft developments.
Keywords
Propulsion System; Flight Test;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
연도 인용수 순위
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