High pressure thermal decomposition behavior and relation to burning rate of catalyzed nitrate propellant

Ning fei Wang*, Zi ru Liu, Liang Wang

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

3 Citations (Scopus)

Abstract

The burning and high pressure thermal decomposition behavior of a typical nitrate propellant with and without catalysts was studied. Lead salt and copper salt moved up the thermal pyrolysis at 5 MPa, but carbon black did not. Lead salt and copper salt and carbon black increased this trend and also increased the reaction rate of nitrate propellants in temperature scope from 191.7 °C to 239.5 °C, and this is the reason of the burning rate increase. ΔH/ΔT had some relation to the burning rate. The higher the ΔH/ΔT, the higher the burning rate.

Original languageEnglish
Pages (from-to)74-78
Number of pages5
JournalTuijin Jishu/Journal of Propulsion Technology
Volume21
Issue number6
Publication statusPublished - Dec 2000
Externally publishedYes

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