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NTIS 바로가기한국추진공학회지 = Journal of the Korean Society of Propulsion Engineers, v.17 no.1, 2013년, pp.89 - 96
문인상 (한국항공우주연구원 미래로켓연구팀) , 문일윤 (한국항공우주연구원 미래로켓연구팀) , 하성업 (한국항공우주연구원 미래로켓연구팀)
Combustion pressures were measured to study combustion stability for an oxygen rich preburner by both of static and dynamic pressure sensors. The resolutions of each static and dynamic pressure sensor are the 1,000 Hz and 25,600 Hz, respectively. The nominal combustion pressure of the preburner was ...
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