Hexanitrohexaazaisowurtzitane
| Hexanitrohexaazaisowurtzitane | |
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2,4,6,8,10,12-Hexanitro-2,4,6,8,10,12-hexaazaisowurtzitane[citation needed] |
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Other names
CL-20 |
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| Identifiers | |
| Abbreviations | CL-20, HNIW |
| CAS number | 135285-90-4 |
| PubChem | 9889323, 11048432 (3R,9R)-dodec, 11419235 (3R,5S,9R,11S)- dodec |
| ChemSpider | 8064994 |
| Jmol-3D images | Image 1 Image 2 |
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| Properties | |
| Molecular formula | C6N12H6O12 |
| Molar mass | 438.1850 g mol-1 |
| Exact mass | 438.022813716 g mol-1 |
| Explosive data | |
| Explosive velocity | 9.38 km s-1 |
| Except where noted otherwise, data are given for materials in their standard state (at 25 °C, 100 kPa) |
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| Infobox references | |
2,4,6,8,10,12-hexanitro-2,4,6,8,10,12-hexaazaisowurtzitane, also called HNIW, and CL-20, is a nitroamine explosive with the formula C6H6N12O12, developed by the China Lake facility, primarily to be used in propellants. It has a better oxidizer-to-fuel ratio than conventional HMX or RDX. It produces 20% more energy than traditional HMX-based propellants, and is widely superior to conventional high-energy propellants and explosives.
While most development of CL-20 has been fielded by the Thiokol Corporation, the US Navy (through ONR) has also been interested in CL-20 for use in rocket propellants, such as for missiles, as it has lower observability characteristics (e.g., less visible smoke).[1]
CL-20 has not yet been fielded in any production weapons system, but is presently undergoing testing for stability, production capabilities, and other weapons characteristics.
[edit] Synthesis
It is made by reacting hexabenzylhexaazaisowurtzitane with acetic anhydride yielding dibenzyltetraethanoylhexaazaisowurtzitane, which is then reacted with nitronium tetrafluoroborate and nitrosonium tetrafluoroborate, resulting in HNIW.
[edit] See also
- 2,4,6-Tris(trinitromethyl)-1,3,5-triazine
- 4,4’-Dinitro-3,3’-diazenofuroxan (DDF)
- Heptanitrocubane (HNC)
- HHTDD
- Octanitrocubane (ONC)