Aeronautical and Space Sciences Japan
Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663
 
Fundamental Combustion Characteristics of Ethanol/Liquid Oxygen Rocket Engine Combustor with Planar Pintle-type Injector
Kazuki SAKAKI
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Keywords: Rocket Engine, Pintle Injector, Optical Measurement, Combustion Stability
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2019 Volume 67 Issue 2 Pages 41

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