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Improving the Combustion Performance of a Hybrid Rocket Engine using a Novel Fuel Grain with a Nested Helical Structure
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Effect of Combustion Chamber Geometrical Parameters on the Decomposition and Combustion Characteristics of an

Yangyang Hou1, Yusong Yu1, Xuhui Liu2

  • 1Hydrogen Energy and Space Propulsion Laboratory, School of Mechanical, Electronic and Control Engineering, Beijing Jiaotong University, Beijing 100044, China.

Micromachines
|April 23, 2022
PubMed

Keywords:
ammonium dinitramidecatalytic combustionchamber geometrical parametersgreen propellant

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