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Thermochemical and energy characteristics of N-(2,2,2-trinitroethyl)aminoand N-(2,2,2-trinitroethyl) nitroamino-derivatives of asidotriazines
D. B. Lempert,
A. I. Kazakov,
A. V. Nabatova,
A. G. Korepin,
A. V. Shastin Institute of Problems of Chemical Physics (IPCP), Russian Academy of Sciences, 142432, Chernogolovka, Russia
Abstract:
The standard enthalpies of formation were experimentally measured for four compounds: 4,6-diazido-N-(2,2,2-trinitroethyl)-1,3,5-triazine-2-amine, 6-azido-N
$^2$, N
$^4$-bis(2,2,2-trinitroethyl)-1,3,5-triazine-2,4-diamine, 6-azido-N
$^2$, N
$^4$-dinitro-N
$^2$, N
$^4$-bis(2,2,2- trinitroethyl)-1,3,5-triazine-2,4-diamine, and N
$^2$, N
$^4$, N
$^6$-trinitro-N
$^2$, N
$^4$, N
$^6$-tris(2,2,2-trinitroethyl)-1,3,5-triazine-2,4,6-triamine – 690.1
$\pm$ 5.9, 326.2
$\pm$ 13.6, 630.1
$\pm$ 6.1, 415.9
$\pm$ 9.3 kJ/mol, respectively. Based on these values, the energy equivalent of replacing the hydrogen atom and the azido group by trinitroethylamine and trinitroethylnitramine groups in triazine and azido-substituted derivatives of triazine. Calculations have shown that 6-azido-N
$^2$, N
$^4$-dinitro-N
$^2$, N
$^4$-bis(2,2,2-trinitroethyl)-1,3,5-triazine-2,4-diamine, and N
$^2$, N
$^4$, N
$^6$-trinitro-N
$^2$, N
$^4$, N
$^6$-tris(2,2,2-trinitroethyl)-1,3,5-triazine-2,4,6-triamine with an oxygen supply ratio greater than 1.0 can be used as the basis for designing compositions with a low aluminum content and with a specific impulse of 257–260 s.
Keywords:
4,6-diazido-N-(2,2,2-trinitroethyl)-1,3,5-triazine-2-amine, 6-azido-N$^2$, N$^4$-bis(2,2,2-trinitroethyl)-1,3,5-triazine-2,4-diamine, 6-azido-N$^2$, N$^4$-dinitro-N$^2$, N$^4$-bis(2,2,2- trinitroethyl)-1,3,5-triazine-2,4-diamine, and N$^2$, N$^4$, N$^6$-trinitro-N$^2$, N$^4$, N$^6$-tris(2,2,2-trinitroethyl)-1,3,5-triazine-2,4,6-triamine, specific enthalpy of formation, composite solid rocket fuel, specific Impulse.
UDC:
541.11:547.235.5
Received: 28.08.2018
Revised: 25.10.2018
Accepted: 28.11.2018
DOI:
10.15372/FGV20200108