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http://dx.doi.org/10.5139/JKSAS.2012.40.8.726

Design for Spin/Stall Recovery Parachute System of Turbo-prop Airplane  

Lee, Dong-Hun (한국항공우주산업(주) 비행계측팀)
Nho, Byung-Chan (한국항공우주산업(주) 비행계측팀)
Kang, Myung-Kag (한국항공우주산업(주) 비행계측팀)
Kang, Gyeong-Woo (한국항공우주산업(주) 비행계측팀)
Lee, Ju-Ha (한국항공우주산업(주) 비행계측팀)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.40, no.8, 2012 , pp. 726-736 More about this Journal
Abstract
This paper deals with Spin/Stall Recovery Parachute System from design to ground taxiing stage which would be deployed on the high speed taxi of turbo-prop airplane. In detail design phase, design parameters- riser length, parachute type, size, porosity, parachute canopy filling time, and deployment method- were considered based on the analytical disciplines such as aerodynamics, structures, and stability & control. Before the installation of Spin/Stall Recovery System of turbo-prop airplane, all control functions of this system were validated by the SBTB(System Breakout Test Box) in the laboratory. SBTB was used to confirm if it can detect faults, and simulate the firing of pyrotechnic devices that control the deployment and jettison of it. Once confirmed normal operation, deployment of parachute on the high speed taxiing were performed.
Keywords
Spin/Stall Recovery; Parachute; KC-100;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
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