BIS(CYCLO-HEXAMETHYLENEDITHIOCARBAMATO)GOLD(III) HYDRODINITRATE: PREPARATION, SUPRAMOLECULAR SELF-ASSEMBLY OF A THREE-DIMENSIONAL PSEUDO-POLYMERIC ARCHITECTURE AND THERMAL BEHAVIOR
A new crystalline ionic gold(III) complex has been prepared and characterised using FT-IR spectroscopy, single-crystal XRD analysis and simultaneous thermal analysis. The target compound was obtained by а reaction between alcohol solutions of gold(III) nitrate, acidified with nitric acid to pH 2.0, and sodium hexamethylenedithiocarbamate. When the inorganic by-products of the reaction were removed, the complex was crystallised from acetone. Under conditions of slow evaporation of the solvent at room temperature, yellow transparent plate-like crystals were isolated. By XRD in the studied compound, the central gold atom bidentately coordinates two dithiocarbamate ligands forming cationic bis(N,N-cyclo-hexamethylenedithiocarbamato-S,S')gold(III), while the anionic moiety is represented by a hydrodinitrate ion. It was established that numerous non-valent interactions play the main role in the formation of the crystal structure of the complex. Structurally non-equivalent bis(N,N-cyclo-hexamethylenedithiocarbamato-S,S')gold(III) complex cations (cations A and B having Au(1) and Au(2) atoms, respectively) are combined via paired interionic secondary Au…S bonds, forming linear cationic chains […A…B…] oriented along the crystallographic b axis. In the additional binding of non-equivalent cations A and B, non-classical hydrogen C–H…S bonds also participate. In discrete hydrodinitrate anions, two structurally nonequivalent nitrate groups are linked by a hydrogen bond, the position of the hydrogen between the O…O atoms is not localized. Subsequent structural ordering of the gold(III) complex is achieved due to multiple hydrogen C–H…O bonds, which combine all ionic structural units of the compound, forming a 3D-pseudopolymeric framework and stabilising its supramolecular architecture. The thermal behaviour of the complex was studied in an argon atmosphere using the STA technique, which involves parallel recording of thermogravimetry and differential scanning calorimetry curves. The only final product of the multi-stage process of thermal destruction of the complex is the recovered highly dispersed metallic gold. For citation: Bredyuk O.A., Rodina T.A., Smolentsev A.I., Ivanov A.V. Bis(cyclo-hexamethylenedithiocarbamato)gold(III) hydrodinitrate: preparation, supramolecular self-assembly of a three-dimensional pseudo-polymeric architecture and thermal behavior. ChemChemTech [Izv. Vyssh. Uchebn. Zaved. Khim. Khim. Tekhnol.]. 2026. V. 69. N 6. P. 52-62. DOI: 10.6060/ivkkt.20266906.6986.
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120
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A fixation mode of gold from solutions using heterogeneous reaction of cadmium dicyclohexyl dithiophosphate with H[AuCl4]. Structural and (13C, 31P) CP/MAS NMR studies and thermal behaviour of crystalline polymeric gold(I) dicyclohexyl dithiophosphate and bis(dicyclohexylthiophosphoryl) disulphide
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Two structural types of dithiocarbamato-chlorido complexes of mercury(II): Preparation, supramolecular self-assembly, solid-state 13C and 15N NMR characterisation and thermal behaviour of pseudo-polymeric compounds of [Hg2(S2CNBu2)2Cl2] and [Hg4(S2CNiBu2)6][Hg2Cl6
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12
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1
- 10.1007/978-981-19-1388-4_6
- May 25, 2022
A typical solid propellant gas generator upon ignition will generate gas-phase combustion products and particulates that leave the generator through an exhaust line. The combustion products are at high pressure and temperature that can be tapped from the gas chamber to control the actuator system. This paper aims to investigate the Ammonium Nitrate (AN)-based gas generator propellants which are most suitable for low flame temperature and chlorine-free combustion products. Ammonium Nitrate is useful for slower burning rate and low flame temperature. Hydroxyl Terminated Polybutadiene (HTPB) was used as a binder and fuel, added to the oxidizer (AN). The ignitability of the propellants is increased by adding certain additives such as Ammonium Dichromate (ADC) and Guanidine Nitrate (GN) in the propellants, which have been studied. Five different propellant compositions were made and analyzed the effect of ammonium dichromate on propellants. Adiabatic flame temperature for the compositions has been determined by using C PROP-SHELL and it was obtained for a constant chamber pressure of 40 bar. For thermal analysis, STA (Simultaneous Thermal Analysis) was used to determine decomposition temperature from the DSC curve and mass loss from the TG curve. Each sample was heated from 30 °C to 600 °C at a heating rate of 27 K/min, and initial decomposition temperature and exothermic peak values were found. The change in mass of a sample with respect to temperature and time in the controlled atmosphere was measured by TGA. The influence of ADC and GN on the decomposition and thermal behavior of propellants has been investigated through this work.KeywordsHydroxyl Terminated Polybutadiene (HTPB)Ammonium Nitrate (AN)Ammonium Dichromate (ADC)Guanidine Nitrate (GN)Toluene Diisocyanate (TDI)Dioctyladipate (DOA)Differential Scanning calorimetry (DSC)Thermogravimetric Analysis (TGA)
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33
- 10.3390/pharmaceutics15061596
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35
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31
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27
- 10.1007/s10973-016-5249-5
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Manganese ferrite nanopowder was prepared by a new solvothermal method, using 1,2 propanediol as solvent and KOH as precipitant. The as-synthesized powder, by solvothermal treatment in autoclave at 195 °C, for 12 h, consisted of fine manganese ferrite nanoparticles. The further thermal treatment of the initial manganese ferrite powder to higher temperature resulted in manganese ferrite decomposition due to Mn(II) oxidation to Mn(III), as observed by X-ray diffraction. FT-IR spectroscopy has evidenced that the oxidation takes place even at 400 °C. The oxidation of Mn(II) to Mn(III) was studied by TG/DSC simultaneous thermal analysis. It was shown that Mn(II) oxidation takes place in a very small extent up to 400 °C. The main oxidation step occurs around 600 °C, when a clear mass gain is registered on TG curve, associated with a sharp exothermic effect on DSC curve. The exothermic effect is smaller in case of the powder annealed at 400 °C, confirming the superficial oxidation of Mn(II) up to 400 °C. In order to avoid Mn(II) oxidation, the powder obtained at 400 °C was further annealed at 800 °C in argon atmosphere, without degassing, when manganese ferrite MnFe2O4 was obtained as major crystalline phase (69 %). All manganese ferrite powders showed a superparamagnetic behavior, with maximum magnetization of 51 emu g−1 in case of the as-synthesized powder, characteristic of magnetic ferrite nanopowders.