한국전산유체공학회:학술대회논문집
- 2002.10a
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- Pages.1-7
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- 2002
Liquid Rocket Regerative Cooling
액체로켓의 재생냉각
Abstract
Liquid rocket regenerative cooling design procedure is introduced with the example of the 250 kg thrust, LOx/kerocine experimental test rocket system. The presentation may be useful for numerical analysists who have limited experiences with real rocket system.
Keywords