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Improving the Combustion Performance of a Hybrid Rocket Engine using a Novel Fuel Grain with a Nested Helical Structure

DOI :

10.3791/61555-v

January 18th, 2021

January 18th, 2021

5,292 Views

1Institute of Mechanics, Chinese Academy of Sciences, 2School of Engineering Science, University of Chinese Academy of Sciences

A technique utilizing a solid fuel grain with a novel nested helical structure to improve the combustion performance of a hybrid rocket engine is presented.

Tags

Combustion Performance

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