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http://dx.doi.org/10.5139/JKSAS.2011.39.4.378

Temperature and Pressure Measurement on the Flame Deflector during KSLV-I Flight Tests  

Jung, Il-Hyung (한국항공우주연구원 발사대개발팀)
Moon, Kyung-Rok (한국항공우주연구원 발사대개발팀)
Kang, Sun-Il (한국항공우주연구원 발사대개발팀)
An, Jae-Chel (한국항공우주연구원 발사대개발팀)
Ra, Seung-Ho (한국항공우주연구원 발사대개발팀)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.39, no.4, 2011 , pp. 378-384 More about this Journal
Abstract
During the flight test of KSLV-I, various sensors are installed in the launch pad and the flame deflector to measure the flame characteristics and their influences on the launch complex when a launch vehicle lifts off. Parameter Measurement System is responsible for acquiring the above flight test data. The measurement methodology such as the configuration of measurement system, sensor locations and data acquisition procedures are presented. And this paper compares and explains the characteristics of data sets measured during two flight tests.
Keywords
KSLV-I; Launch Complex; Technological Equipment of Parameter Measurement System; Flame Deflector;
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