| Literature DB >> 35479050 |
Dmitry A Gulyaev1, Michael S Klenov1, Aleksandr M Churakov1, Yurii A Strelenko1, Ivan V Fedyanin2,3, David B Lempert4, Ekaterina K Kosareva5, Tatiana S Kon'kova5, Yurii N Matyushin5, Vladimir A Tartakovsky1.
Abstract
The strategy for the synthesis of substituted [(3-nitro-1H-1,2,4-triazol-1-yl)-NNO-azoxy]furazans 4-7, in which the distal nitrogen of the azoxy group is bonded to the nitrogen atom of the azole ring, includes, firstly, the reaction of 1-amino-3-nitro-1H-1,2,4-triazole with 2,2,2-trifluoro-N-(4-nitrosofurazan-3-yl)acetamide in the presence of dibromisocyanuric acid followed by removing of the trifluoroacetyl protecting group to afford aminofurazan (4). Transformation of the amino group in the latter made it possible to synthesize the corresponding nitro (5), azo (6), and methylene dinitramine (7) substituted furazans. The compounds synthesized are thermally stable (decomposition onset temperatures 147-228 °C), exhibit acceptable densities (1.77-1.80 g cm-3) and optimal oxygen balance (the oxidizer excess coefficients α = 0.42-0.71). Their standard enthalpies of formation (576-747 kcal kg-1) were determined experimentally by combustion calorimetry and these compounds have been estimated as potential components of solid composite propellants. In terms of the specific impulse level, model solid composite propellant formulations based on nitro and methylene dinitramine substituted furazans 5 and 7 outperform similar formulations based on CL-20 by 1-4 s, and formulations based on HMX and RDX by 5-8 s. This journal is © The Royal Society of Chemistry.Entities:
Year: 2021 PMID: 35479050 PMCID: PMC9036641 DOI: 10.1039/d1ra03919a
Source DB: PubMed Journal: RSC Adv ISSN: 2046-2069 Impact factor: 4.036
Fig. 1Two different modes of connection of terminal N atom of the azoxy group with heterocycles: C–N linking (A, 1, 3) and N–N linking (B, 2, 4).
Scheme 1Synthesis of substituted [(3-nitro-1H-1,2,4-triazol-1-yl)-NNO-azoxy]furazans 4–7. Reagents and conditions: (i) DBI, MeCN, 0 °C, 2 h; (ii) CF3CO2H, MeOH, H2O, 0 °C, 12 h; (iii) N2O5 (10 equiv.), MeCN, −20 °C, then 0 °C, 14 days; (iv) KMnO4, HCl, H2O, 55 °C, 4 h; (v) CH2O, H2SO4, H2O, 1,4-dioxane, 20 °C, 40 min; (vi) N2O5 (2 equiv.), MeCN, −20 °C, then 0 °C, 1 h.
Fig. 514N and 15N NMR spectra of methylene dinitramine 7.
Standard thermochemical characteristics for compounds 4–7
| Compound |
|
|
|
|---|---|---|---|
| 4 | 2587.0 ± 1.5 | 619.4 ± 0.4 | 140.7 ± 0.4 |
| 5 | 2110.2 ± 2.0 | 566.5 ± 0.5 | 156.1 ± 0.5 |
| 6 | 2482.3 ± 2.7 | 1177.7 ± 1.3 | 356.9 ± 1.3 |
| 7 | 2290.2 ± 3.5 | 1326.3 ± 2.0 | 343.2 ± 2.0 |
Energy of combustion under bomb conditions.
Standard enthalpy of combustion.
Standard enthalpy of formation.
Physical and detonation properties of compounds 4–7 in comparison with RDX
| Formula | 4 | 5 | 6 | 7 | RDX |
|---|---|---|---|---|---|
| C4H3N9O4 | C4HN9O6 | C8H2N18O8 | C9H4N20O12 | C3H6N6O6 | |
| FW [g mol−1] | 241 | 271 | 478 | 584 | 222 |
|
| 1.78 | 1.80 | 1.77 | 1.79 | 1.82 |
|
| 200 | 117 | — | — | 204 |
|
| 200 | 228 | 184 | 147 | 204 |
|
| 0.42 | 0.71 | 0.47 | 0.6 | 0.67 |
|
| 52.28 | 46.49 | 52.72 | 47.95 | 37.84 |
|
| −9.96 | 8.86 | −3.35 | 2.74 | 0 |
|
| −36.51 | −14.76 | −30.13 | −21.92 | −21.62 |
|
| +584 | +576 | +747 | +588 | +72 |
|
| 8.71 | 8.83 | 8.69 | 8.79 | 8.96 |
| 8.75 | |||||
|
| 33.9 | 36.2 | 34.0 | 35.5 | 36.6 |
| 35.0 | |||||
|
| 1425 | 1609 | 1539 | 1570 | 1479 |
| 1512 | |||||
| IS [J] | 9 | 2 | 1 | 2 | 7.5 |
| FS [N] | 210 | 35 | 23 | 65 | 120 |
Formula weight.
Density measured by powder diffraction at 298 K.
Melting temperature (DSC).
Decomposition temperature (extrapolated onset temperature at a heating rate of 5 °C min−1).
Oxidizer excess coefficient.
Nitrogen content.
Oxygen balance (based on CO).
Oxygen balance (based on CO2).
Experimentally measured standard enthalpy of formation.
Detonation velocity.
Detonation pressure.
Heat of detonation.
Impact sensitivity.
Friction sensitivity.
Density measured by gas pycnometer at 298 K.
Calculated with Shock and Detonation (S&D) Version 4.5.
Ref. 25.
Fig. 6Formulations of the organic energetic filler + the active binder (18 vol%, 14.5–15.5 wt%) + aluminum. Dependence of Isp on the kind of the organic energetic filler and on the content of aluminum in the formulation.
The main energetic characteristics of binary formulations containing the organic energetic filler + the active binder (18 vol%, 14.5–15.5 wt%)
| Organic energetic filler | wt% of organic energetic filler | Density, g cm−3 | Temperature in the combustion chamber, K |
|
|---|---|---|---|---|
| 5 | 84.75 | 1.761 | 3680 |
|
| 7 | 84.55 | 1.736 | 3580 |
|
| CL-20 | 86.20 | 1.944 | 3450 | 255.7 |
| 6 | 84.47 | 1.728 | 3540 | 252.3 |
| HMX | 85.35 | 1.832 | 3175 | 251.0 |
| RDX | 84.75 | 1.761 | 3180 | 251.1 |
| 4 | 84.55 | 1.736 | 3080 | 240.6 |
Fig. 7Formulations of the organic energetic filler + the active binder (18 vol%, 14.5–15.5 wt%) + ammonium perchlorate (AP). Dependence of Isp on the kind of the organic energetic filler and on the content of AP in the formulation.