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Fizika Goreniya i Vzryva, 2020 Volume 56, Issue 4, Pages 104–111 (Mi fgv699)

This article is cited in 9 papers

Thermochemical and energy characteristics of N-(2,2-bis(methoxy-nno-azoxy) ethyl)nitramine

I. N. Zyuzin, D. B. Lempert, A. V. Nabatova, A. I. Kazakov

Institute of Problems of Chemical Physics, Russian Academy of Sciences, 142432, Chernogolovka, Russia

Abstract: The standard enthalpies of formation of 1,1-bis(methoxy-NNO-azoxy)-3-nitro-3-azabutane and 1,1,8,8-tetrakis (methoxy-NNO-azoxy)-3,6-dinitro-3,6-diazaoctane were experimentally determined to be 87.7 $\pm$ 3.9 and 283.8 $\pm$ 6.2 kJ/mol, respectively. Calculations have shown that solid composite propellants containing these two compounds as gasifying components in metal-free compositions based on an active binder and ammonium perchlorate are inferior in the highest achievable effective impulse at the third stage of the rocket system $I_{ef}$ (3) to compositions based on HMX, but in designing special compositions with a limited content of organic explosive (not higher than 30–35%), these two compounds provide 5–10 s higher values of $I_{ef}$ (3) than when using HMX.

Keywords: 1-bis(metho-xy-NNO-azoxy)-3-nitro-3-azabutane, 1,1,8,8-tetrakis (methoxy-NNO-azoxy)-3,6-dinitro-3,6-diazaoctane, alkoxy-NNO-azoxy compounds, nitramines, enthalpy of combustion, enthalpy of formation, solid composite propellants, specific impulse.

UDC: 541.11:547.235.5:547.416

Received: 19.06.2019
Revised: 02.08.2019
Accepted: 28.08.2019

DOI: 10.15372/FGV20200410


 English version:
Combustion, Explosion and Shock Waves, 2020, 56:4, 464–470

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© Steklov Math. Inst. of RAS, 2024