Thermal reaction characteristics of the boron used in the fuel-rich propellant-Reference-Cited by-同舟云学术

Thermal reaction characteristics of the boron used in the fuel-rich propellant

Published:2013-04-06 Issue:3 Volume:114 Page:1057-1068
ISSN:1388-6150
Container-title:Journal of Thermal Analysis and Calorimetry
language:en
Short-container-title:J Therm Anal Calorim

Author:

Liu Lin-lin,He Guo-qiang,Wang Ying-hong

Publisher

Springer Science and Business Media LLC

Link

http://link.springer.com/content/pdf/10.1007/s10973-013-3119-y.pdf

Reference10 articles.

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2. Kuo KK. Combustion of boron-based solid propellants and solid fuels. Boca Raton: CRC Press; 1993.

3. King MK. Ignition and combustion of boron particles and clouds. J Spacecraft. 1982;19:294–306.

4. Zhou W. Numerical study of multi-phase combustion: ignition and combustion of ail isolated boron particle in fluorinated environments: Candidacy. Ph.D. Thesis. Princeton: Princeton University; 1998.

5. Yeh CL, Kuo K. Ignition and combustion of boron particles. Prog Energy Combust Sci. 1996;2:511–41.

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