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 language | English |
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Pages (from-to) | 74-78 |
Number of pages | 5 |
Journal | Tuijin Jishu/Journal of Propulsion Technology |
Volume | 21 |
Issue number | 6 |
Publication status | Published - Dec 2000 |
Externally published | Yes |