Abstract
The thermal decomposition performance and compatibility of 4, 10-dinitro-2, 6, 8, 12-tatraoxa-4, 10-diazatatracyclo [5, 5, 0, 05, 9, 03, 11]-decane (TEX) with main components of propellants such as cyclotrimethylenetrinitramine(RDX), N-nitrodihydroxyethylaminedinitrate(DINA), nitrocellulose (NC), absorbentia(NC+NG), diethylphthalate(DEP), leadphthalate(Φ-Pb) and aluminium powder(micron order) were studied by differential scanning calorimetry(DSC). The results show that TEX is relatively stable to heat, the binary system of TEX was compatible with RDX, Φ-Pb, NC, DINA and aluminium powder, and was slightly sensitive with absorbentia(NC+NG) and NC. Thus TEX can be used as component in propellants.
| Original language | English |
|---|---|
| Pages (from-to) | 66-69 |
| Number of pages | 4 |
| Journal | Huozhayao Xuebao/Chinese Journal of Explosives and Propellants |
| Volume | 38 |
| Issue number | 2 |
| DOIs | |
| Publication status | Published - 1 Apr 2015 |
Keywords
- 4,10-dinitro-2,6,8,12-tatraoxa-4,10-diazatatracyclo[5,5,0,0, 0]-decane
- Compatibility
- Differential scanning calorimetry
- Physical chemistry
- Propellant
- TEX
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