Study on the heat transfer characteristics of regenerative cooling for LOX/LCH4 variable thrust rocket engine
It is a challenging task to investigate the regenerative cooling of the variable thrust LOX/LCH4 expander cycle rocket engine. The decreasing methane mass flow rate leads to the two-phase instability in the regenerative cooling channels (RCC) for low engine thrust. In this study, the geometric dimen...
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Published in | Case studies in thermal engineering Vol. 28; p. 101664 |
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Main Authors | , , , , , , |
Format | Journal Article |
Language | English |
Published |
Elsevier Ltd
01.12.2021
Elsevier |
Subjects | |
Online Access | Get full text |
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