EFFECT OF CR2O3 ON THE BURNING CHARACTERISTICS OF AN / MGAL – BASED COMPOSITE SOLID PROPELLANTS

Authors

  • K. Kamunur Al-Farabi Kazakh National University, Almaty, Kazakhstan; Institute of Combustion Problems, Almaty, Kazakhstan
  • J.M. Jandosov Al-Farabi Kazakh National University, Almaty, Kazakhstan; Institute of Combustion Problems, Almaty, Kazakhstan
  • R.G. Abdulkarimova Al-Farabi Kazakh National University, Almaty, Kazakhstan; Institute of Combustion Problems, Almaty, Kazakhstan
  • M.K. Atamanov Al-Farabi Kazakh National University, Almaty, Kazakhstan; Institute of Combustion Problems, Almaty, Kazakhstan
  • Z.A. Mansurov Al-Farabi Kazakh National University, Almaty, Kazakhstan; Institute of Combustion Problems, Almaty, Kazakhstan
  • Keiichi Hori Japan Aerospace Exploration Agency(JAXA), Sagamihara, ,Japan

Keywords:

AN/MgAl - based solid propellant,, catalytic combustion,, burning rate,, pressure vessels,, high-speed camera

Abstract

In this work studied on the burning characteristics of AN / MgAl – based solid propellant catalytic combus-tion with the addition of Cr2O3. The addition Cr2O3 improves ignition at low pressures. However, the addi-tion of Cr2O3 increased burning rate, the use of mechanical alloy MgAl as an oxidizer allowed propellant ignited at low temperatures. Samples were burned in the combustion chamber under nitrogen pressure 1MPa, 3MPa and 5MPa with a video camera determined burning rate

References

(1) Kohga, M., & Okamoto, K. (2011). Thermal decomposition behaviours and burning characteristics of ammonium nitrate/polytetrahydrofuran/glycerin composite propellant. Combustion and Flame, 158(3), 578–582.

(2) Chakravarthy, S.R., Freeman, J.M., Price, E.W., & Sigman, R.K. (2004). Combustion of propellants with ammonium dinitramide. Propellants, Explosives, Pyrotechnics, 29(4), 220-230.

(3) Manelis, G.B., & Lempert, D.B. (2009). Ammonium nitrate as an oxidizer in solid composite propellants. Progress in Propulsion Physics, 1, 81-96.

(4) Naya, T., & Kohga, M. (2013). Influences of particle size and content of HMX on burning characteristics of HMX-based propellant. Aerospace Science and Technology, 27(1), 209–215.

(5) Kohga, M., & Nishino, S. (2009). Burning characteristics of ammonium nitrate-based composite propellants supplemented with ammonium dichromate. Propellants, Explosives, Pyrotechnics, 34(4), 340–346.

(6) Rodić, V. (2012). Effect of titanium (IV) oxide on composite solid propellant properties. Scientific Technical Review, 62(3-4), 21-27.

(7) Naya, T., & Kohga, M. (2013). Burning characteristics of ammonium nitrate-based composite propellants supplemented with MnO2. Propellants, Explosives, Pyrotechnics, 38, 87–94.

(8) Naya, T., & Kohga, M. (2013). Burning characteristics of ammonium nitrate-based composite propellants supplemented with Fe2O3. Propellants, Explosives, Pyrotechnics, 38(4), 547–554.

(9) Kohga, M., & Naya, T. (2015). Thermal decomposition behaviors and burning characteristics of AN/RDX-based composite propellants supplemented with MnO2 and Fe2O3. Journal of Energetic Materials, 33(4), 288-304.

(10) Aly, Y., Schoenitz, M., & Dreizin, E.L. (2013). Ignition and combustion of mechanically alloyed Al–Mg powders with customized particle sizes. Combustion and Flame, 160, 835–842.

(11) Murata, H., Azuma, Y., Tohara, T., et al. (2000). The effect of magnalium (Mg-Al alloy) on combustion characteristics of ammonium nitrate-based solid propellant. Science and Technology of Energetic Materials, 61(2), 58–66.

(12) Shoshin, Y.L., Mudryy, R.S., & Dreizin, E.L. (2002). Preparation and characterization of energetic Al-Mg mechanical alloy powders. Combustion and Flame, 128(3), 259-269.

(13) Habu, H., & Hori, K. (2006). The burning rate characteristics of magnalium (Mg/Al)-AP based solid propellant. Science and Technology of Energetic Materials, 67(6), 187-192.

(14) Lee, J.K., & Kim, S.K. (2011). Effect of CaO addition on the ignition resistance of Mg-Al alloys. Materials Transactions, 52(7), 1483-1488.

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Published

2016-09-25

How to Cite

Kamunur, K., Jandosov, J., Abdulkarimova, R., Atamanov , M., Mansurov, Z., & Hori, K. (2016). EFFECT OF CR2O3 ON THE BURNING CHARACTERISTICS OF AN / MGAL – BASED COMPOSITE SOLID PROPELLANTS. Combustion and Plasma Chemistry, 14(3), 189-194. https://www.cpc-journal.kz/index.php/cpcj/article/view/510