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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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Ignition and flame stabilization of a strut-jet RBCC combustor with small rocket exhaust

Jichao Hu1, Juntao Chang1, Wen Bao1

  • 1Harbin Institute of Technology, Xidazhi Street No. 92, Harbin, Heilongjiang 150001, China.

Thescientificworldjournal
|March 1, 2014
PubMed

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