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http://dx.doi.org/10.6108/KSPE.2022.26.6.010

Development of Design Code for Oxidizer-Rich Preburner of Staged Combustion Cycle Engine Using Cantera  

Si-Yoon Kang (Aerospace System Engineering, University of Science and Technology)
Seong-Ku Kim (Combustion Chamber Team, Korea Aerospace Research Institute)
Chulsung Ryu (Combustion Chamber Team, Korea Aerospace Research Institute)
Insang Moon (KARI Academy Team, Korea Aerospace Research Institute)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.26, no.6, 2022 , pp. 10-20 More about this Journal
Abstract
The present study developed a design code for preburner of staged combustion cycle engines, which calculates preburnt gas at high-pressure oxidizer-rich conditions and predicts conjugate heat transfer and hydraulics of cryogenic fluid flow through cooling passages. It has been written based on the open-source library Cantera, into which this study has incorporated new source codes to predict correctly non-ideal thermodynamics and transport anomalies of the cryogenic fluid. For a preburner of 100 tonf-class booster engine currently under preliminary design, the present code demonstrated predictive capability and usability as a design code by comparing with CFD simulation.
Keywords
Staged-Combustion Cycle; Oxidizer-Rich Preburner; Real-Fluid Model; Conjugated Heat Transfer;
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