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Byung-Hun Kim

Chungnam National University

7

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12

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Analysis of Dynamic Characteristics and Performance of Solenoid Valve for Pressurization Propellant Tank

2013
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Modeling the Prediction of Helium Mass Requirement for Propellant Tank Pressurization

2012 Journal of Spacecraft and Rockets
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Estimation of Heat Transfer Coefficient at the Upper Layer of Cryogenic Propellant

2012
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The Rubber Performance Evaluation for Kick Motor Flexible Seal

2011 Journal of The Korean Society for Aeronautical & Space Sciences
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Required Pressurant Mass for Cryogenic Propellant Tank with Pressurant Temperature Variation

2010 Journal of The Korean Society for Aeronautical & Space Sciences
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Prediction for Slag Mass Accumulation in the Kick Motor

2009
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