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Computational Determination of the Specific Impulse of Solid Rocket Propellant Compositions of closo-Dodecaborate ([B₁₂H₁₂]2‒) Salts with HTPB Binder and Ammonium Perchlorate as an Oxidizer

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Języki publikacji
EN
Abstrakty
EN
Boron (B) powder in elemental form is a very attractive high-energy material and it is a metalloid chemical element. B powder has the second highest heat of explosion of any element that can be adopted as an energetic material in dealing with propellants and explosives. In practical situations, B has problems with ignition and combustion due to the formation of a B₂O₃ layer on its surface. B cannot burn easily; it requires ultra-pure oxygen during the combustion process and also undergoes agglomeration due to which incomplete combustion of the B particles in the propellant composition occurs. Hence in order to address these issues, we introduced closo-dodecaborate ([B₁₂H₁₂]2‒) salts into a solid rocket propellant composition instead of B powder. In the present work, three solid rocket propellant compositions based on closo-dodecaborate salts were theoretically investigated. The specific impulse (Isp) was calculated for three closo-dodecaborate [B₁₂H₁₂]2‒ based propellant compositions using the EXPLO5 code version V6.03. The performance values of the closo-dodecaborate [B₁₂H₁₂]2‒ salts based propellant compositions were compared with those of pure aluminium (Al)-based composite propellant. Using the EXPLO5 code (V6.03); hydroxyl-terminated polybutadiene (HTPB) and ammonium perchlorate (NH₄ClO₄, AP) were used as binder and oxidizer respectively. closo-Dodecaborate salts-HTPB-AP formulations have good theoretical performance; it was observed that the presence of a closo-dodecaborate salt in the propellant composition can lead to very good performance, and they are potential candidates as fuels and/or fuel additives in propellant compositions for missile and rocket applications.
Rocznik
Strony
386--399
Opis fizyczny
Bibliogr. 22 poz., rys., tab., wykr.
Twórcy
  • Advanced Centre of Research in High Energy Materials (ACRHEM), University of Hyderabad, Hyderabad-500046, India
Bibliografia
  • [1] Pang, W.; Fan, X.; Lv, K. The Physicochemical Properties of Boron Powder and Its Application Progress in Fuel Rich Solid Propellant. (in Chinese) J. Winged Missiles 2009, 10: 58-62.
  • [2] Han, L.; Wang, R.; Chen, W.; Wang, Z.; Zhu, X.; Huang, T. Preparation and Combustion Mechanism of Boron-Based High-Energy Fuels. Catalysts 2023, 13(2): paper 378; https://doi.org/10.3390/catal13020378.
  • [3] Pace, K.K.; Jarmowycz, T.A.; Kuo, K.K. Effect of Magnesium-coated Boron Particles on Burning Characteristics of Solid Propellants in High-Rate Cross-Flows. In: Combustion of Boron-based Solid Propellant and Solid Fuels. (Kuo, K.K.; Pein, R.; Eds.) Begell House & CRC Press, Boca Raton/New York, 1993, pp. 332-346; ISBN-13: 978-0849399190.
  • [4] Davis, A. Solid Propellants: The Combustion of Particles of Metal Ingredients. Combust. Flame 1963, 7: 359-367.
  • [5] Pang, W.; Fan, X. Progress in Application of Metal Fuel in Solid Propellants. (in Chinese) Chem. Propellants Polym. Mater. 2009, 7: 1-6.
  • [6] DeLuca, L.T.; Shimada, T.; Sinditskii, V.P.; Calabro, M.; Manzara, A.P. An Introduction to Energetic Materials for Propulsion. In: Chemical Rocket Propulsion. (De Luca, L.; Shimada, T.; Sinditskii, V.; Calabro, M.; Eds.) Springer Aerospace Technology. Springer, Cham, 2017, pp. 3-59; ISBN 978-3-319-27748-6. https://doi.org/10.1007/978-3-319-27748-6_1.
  • [7] Yuan-jun, Z. Progress in the Research of Metal Propellants. J. Propul. Technol. 1981, 3: 66-68.
  • [8] Wei, Z.; Hui, Z.; Ding-qiu, F. Technical Approaches to Improve the Combustion Characteristics of High Energy Fuel Rich Propellants with Boron Particles. Chin. J. Energ. Mater. 1998, 6(4): 179-182.
  • [9] Gany, A. Combustion of Boron-containing Fuels in Solid Fuel Ramjets. In: Combustion of Boron-based Solid Propellant and Solid Fuels. (Kuo, K.K.; Pein, R.; Eds.) Begell House & CRC Press, Boca Raton/New York, 1993, 91-112; ISBN-13: 978-0849399190.
  • [10] Pang, W.; Zhang, J.-Q.; Zhang, Q.-F.; Hu, S.-Q.; Guo, J.-Y. Coating of Boron Particles and Combustion Residue Analysis of Boron-based Solid Propellants. J. Solid Rocket Technol. 2006, 12(2): 204-207.
  • [11] Yang, P. Research on the Combustion of Metal Fuel in Solid Ramjet. J. Propuls. Technol. 1986, 5: 76-79.
  • [12] Koch, C.C.; Scattergood, R.O.; Youssef, K.M.; Chan, E.; Zhu, Y.T. Nanostructured Materials by Mechanical Alloying: New Results on Property Enhancement. J. Mater. Sci. 2010, 45: 4725-4732.
  • [13] Hong-jie, F.; Ning-fei, W.; Da-lin, G. Study on the Combustion Characteristics of Boron Solid Propellant Coatedwith GAP. J. Propuls. Technol. 2002, 23(3): 262-264.
  • [14] Pang, W.; Fan, X.; Zhang, W.; Xu, H.; Li, J.; Li, Y.; Shi, X.; Li, Y. Application of Amorphous Boron Agglomerated with Hydroxyl-terminated Polybutadiene in Fuel Rich Solid Propellant. Propellants Explos. Pyrotech. 2011, 36: 360-366; https://doi.org/10.1002/prep.200900112.
  • [15] Pang, W.; Fan, X. Application Progress of Metal Fuels in Solid Propellants. Chem. Propellants Polym. Mater. 2009, 7: 1-6.
  • [16] Tang, S.Q.; Ding, H.X. Boron Hydrides as Solid Propellant Burning Rate Modifiers of the Latest Progress. (in Chinese) J. Propul. Technol. 1983, 4: 35-49.
  • [17] Zheng, Y.Y.; Wang, M.W. High Burning Rate Modifiers ‒ Polyhedral Boron Hybrid. (in Chinese) Chin. J. Explo. Propellants 1989, 12(3): 32.
  • [18] Gany, A.; David, W.N. Combustion Studies of Metallized Fuels for Solid-Fuel Ramjets. J. Propul. Power 1986, 2: 423-427; https://doi.org/10.2514/3.22924.
  • [19] Suceska, M. EXPLO5 version 6.03. User’s Guide, 2014.
  • [20] Jadhav, P.M.; Patil, J.; Prasanth, H.; Rao, G. Ammonium Dodecahydrododecaborate (NH₄)₂[B₁₂H₁₂]: Hydrogen and Boron Rich Fuel for Jet Propulsion Engines. Cent. Eur. J. Energ. Mater. 2022, 19(2): 158-167; https://doi.org/10.22211/cejem/151579.
  • [21] Rao, M.H.; Muralidharan, K. Syntheses, Characterization and Energetic Properties of closo-(B₁₂H₁₂)2‒) Salts of Imidazolium Derivatives. Dalton. Trans. 2013, 42(24): 8854-8860; https://doi.org/10.1039/C3DT32834A.
  • [22] Rao, M.H.; Muralidharan, K. Closo-Dodecaborate (B₁₂H₁₂)2‒) Salts with Nitrogen Based Cations and Their Energetic Properties. Polyhedron 2016, 115: 105-110; https://doi.org/10.1016/j.poly.2016.03.062.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-abd7b597-1027-4d2d-98c1-927ae3506d9d
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