Effect of combustion gas mass flow rate on carbon/carbon composite nozzle ablation in a solid rocket motor

Li Na Peng, Guo Qiang He, Jiang Li, Lei Wang, Fei Qin

Research output: Contribution to journalArticlepeer-review

65 Scopus citations

Fingerprint

Dive into the research topics of 'Effect of combustion gas mass flow rate on carbon/carbon composite nozzle ablation in a solid rocket motor'. Together they form a unique fingerprint.

Engineering

Material Science