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http://dx.doi.org/10.5139/JKSAS.2015.43.11.1028

Design of Space Launch Vehicle Solenoid Valve for Cryogenic Environment  

Kim, Byunghun (Supply System Team, Korea Aerospace Research Institute)
Han, Sangyeop (Supply System Team, Korea Aerospace Research Institute)
Ko, Youngsung (Dept. of Aerospace Engineering, Chungnam National University)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.43, no.11, 2015 , pp. 1028-1034 More about this Journal
Abstract
Solenoid valves for space launch vehicles require the strict limitations on the size, weight and current consumption comparing to industrial solenoid valves. The preliminary design of a cryogenic and high pressure solenoid valve for propellant tank pressurization which can ensure the operation of solenoid valve under such strict limitation conditions was preformed. The Copper and Constantan materials in coil design have used to prevent the excessive rise of the current at cryogenic state. The measured current of solenoid valve at cryogenic temperature satisfies a design requirement.
Keywords
Solenoid Valve; Coil; Constantan; Cryogenic; Current;
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