Abstract
Residues formed with mass loss of 90.1% and 91.8% from hexanitrohexaazaisowurtzitane (HNIW) at 3 MPa and 216°C were studied by DSC, TG/DSC and FTIR. Residue with mass loss of 90.1% from HNIW contains small amount of remaining nitro group. The remaining nitro group in the residue is eliminated at 220°C when it is proceeded with thermal decomposition. Both the eliminated nitro group residue and the residue with mass loss of 91.8% from HNIW contain the structure of six-membered ring amide. It decomposes at the range of 280-4001 and produce the endothermic peak of DSC, chemical kinetic constants of eliminating reaction of remaining nitro group and cleavage reaction of six-membered ring amide in the residue with mass loss of 90.1% are given through analysis of kinetics for the residue with mass loss of 90.1% respectively.
Original language | English |
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Pages (from-to) | 467-470 |
Number of pages | 4 |
Journal | Tuijin Jishu/Journal of Propulsion Technology |
Volume | 26 |
Issue number | 5 |
Publication status | Published - Oct 2005 |
Keywords
- Dynamics
- High energy propellant
- Infrared spectrum
- Nitramine propellant
- Residue
- Thermal decomposition