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Combustion Characteristics and Mechanism of Boron-based, Fuel-rich Propellants with Agglomerated Boron Powder

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
In order to extend the burning rate of boron-based, fuel-rich solid propellants with agglomerated boron powder, the effects of the boron content, the AP content, and of the magnesium powder content, on the burning rate and pressure exponent have been studied systematically. It has been shown that when the AP content is constant, the burning rate of the propellants increases with an increase in the agglomerated boron content. Furthermore, the burning rate and pressure exponent increase with increasing the contents of AP and magnesium powder. By means of single colour frame amplification photography and combustion wave tests, the combustion mechanism of these propellants has been investigated. It has been shown that the flame of the propellants becomes brighter by increasing the AP content, the dT/dxcp and dT/dxgp of the propellant FR-5 being around 6815 and 5789 °C/mm respectively, higher than those of FR-4, resulting in greater burning rates. The Ts of these propellants is above 683 °C, which is higher than the decomposition peak temperatures of agglomerated boron powder and of propellants (about 649 °C), which indicates that agglomerated boron powder is partially oxidized on the combustion surface, and the heat released from it may be beneficial to the combustion of the propellants.
Rocznik
Strony
575--587
Opis fizyczny
Bibliogr. 12 poz., rys., tab.
Twórcy
autor
  • Science and Technology on Combustion and Explosion Laboratory, Xi’an Modern Chemistry Research Institute, Shaaxi Xi’an 710065, China
autor
  • Xi’an Modern Chemistry Research Institute, Shaaxi Xi’an 710065, China
autor
  • Xi’an Modern Chemistry Research Institute, Shaaxi Xi’an 710065, China
autor
  • Science and Technology on Combustion and Explosion Laboratory, Xi’an Modern Chemistry Research Institute, Shaaxi Xi’an 710065, China
autor
  • Science and Technology on Combustion and Explosion Laboratory, Xi’an Modern Chemistry Research Institute, Shaaxi Xi’an 710065, China
autor
  • Science and Technology on Combustion and Explosion Laboratory, Xi’an Modern Chemistry Research Institute, Shaaxi Xi’an 710065, China
Bibliografia
  • [1] Nieder E.G., Chemical Passivation of Amorphous Boron Powder, US Patent 4 637 847, 1987.
  • [2] Li S.F., Jin R.C., Surface Coating of Boron Powder and Its Effect (in Chinese), Chin. J. Energ. Mater. (Hanneng Cailiao), 1996, 4(3), 102-108.
  • [3] Pang A.M., Zheng J., Xiao J.W., Investigation into the Feasibility of Boron Powder Burning in the Second Combustor of Ducted Rocket Motor (in Chinese), Chin. J. Energ. Mater. (Hanneng Cailiao), 2004, 12 (Suppl.), 185-188.
  • [4] John C., Coating of Boron Particles, US Patent 4 915 753, 1988.
  • [5] Xu H.X., Zhao F.Q., Li Y.H., Effect of Neutralised Boron Powder on the Rheological Property of B/HTPB (in Chinese), Chin. J. Energ. Mater. (Hanneng Cailiao), 2007, 15(4), 341-344.
  • [6] Macri B.J., Process for Making Spheroidal Agglomerates, US Patent 3 646 174 A, 1972.
  • [7] Pang W.Q., Zhang J.Q., Hu S.Q., Dang J.B., Guo J.Y., The Influence of Agglomerated Boron on Burning Rate of Fuel-Rich Solid Propellant (in Chinese), Chin. J. Explos. Propellants (Huozhayao Xuebao), 2006, 29(3), 20-22.
  • [8] Wang Y.H., Li B.X., Hu S.Q., Xiao X.Y., Effect of AP Particle Size and Coating on Combustion of Boron (in Chinese), J. Solid Rocket Technol. (Guti Huojian Jishu), 2004, 27(1), 50-52.
  • [9] Wang Y.H., Li B.X., Zhang X.H., Wu W.E., Study on Burning Surface Sedimentary Deposit of Boron-based Fuel-rich Propellant (in Chinese), J. Solid Rocket Technol. (Guti Huojian Jishu), 2006, 29(2), 120-123
  • [10] Wang Y.H., Li B.X., Hu S.Q., Li J.X., Study on Combustion Mechanism of Fuelrich Propellant Holding Boron Coated with AP (in Chinese), Chin. J. Explos. Propellants (Huozhayao Xuebao), 2004, 27(2), 44-47.
  • [11] Hu S.Q., Li B.X., Wang Y.H., Wei Q., Combustion Characteristics of Boron-based Fuel-rich Propellant at Low Pressure (in Chinese), J. Propul. Technol. (Tuijin Jishu), 2002, 23(6), 518-520.
  • [12] Xu H.X., Zhao F.Q., Li X.Y., Purification of Amorphous Boron Powder with Solvents (in Chinese), Chin. J. Explos. Propellants (Huozhayao Xuebao), 2007, 30(2), 8-12.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-2a66a903-9d6c-4e93-bf56-17018a48a0ad
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