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Isocyanate-free Carboxyl-terminated Polybutadiene and Epoxidised Hydroxyl-terminated Polybutadiene Cross-linking System as a Binder in Solid Heterogeneous Propellants

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Języki publikacji
EN
Abstrakty
EN
Propellants have found applications in many industries. They play an important role primarily in the armaments and space industries. Research and development of propellant technology has been ongoing for many years. The present authors have turned their attention to the aspect of compatibility of new components with isocyanates. As a result of the search for a solution to combine existing binders with new components, they propose using hydroxyl-terminated polybutadiene (HTPB) derivatives as the main binder components. In this way, the basic parameters of the HTPB binder, such as glass transition temperature, and compatibility with the solid components of propellants are retained. The use of an isocyanate-free binder system opens up possibilities for the use of new isocyanatesensitive components. The authors have used two HTPB derivatives to create a new binder system. The combination of carboxyl-terminated polybutadiene (CTPB) and epoxidised HTPB, called EHTPB, allowed the elimination of isocyanates and the retention of good physicochemical properties of the binder. Here they present the method of synthesis of the components, the proportions of polymer and curing agent, and the pot-life. Heterogenic propellants based on CTPB, EHTPB, and ammonium perchlorate (AP) were prepared and the feasibility of such a system was confirmed. A study of the physical and chemical properties of the produced propellants confirmed the possibility of using CTPB and HTPB as a new binder system.
Rocznik
Strony
200--220
Opis fizyczny
Bibliogr. 23 poz., rys., tab., wykr.
Twórcy
  • Warsaw University of Technology, 3 Noakowskiego Street, 00-664 Warsaw, Poland
  • Warsaw University of Technology, 3 Noakowskiego Street, 00-664 Warsaw, Poland
Bibliografia
  • [1] Florczak, B.; Witkowski, W. Prospects for the Development of Solid Heterogeneous Rocket Fuels. (in Polish) Issues of Armament Technology 2006, 98: 67-78.
  • [2] Chmielarek, M.; Sztejter, B.; Kasprzak, P.; Prasuła. P. Effects of Azide-HydroxylTerminated Polybutadiene on the Properties of Solid Heterogeneous Rocket Propellants. Cent. Eur. J. Energ. Mater. 2022, 19(4): 393-408; DOI: 10.22211/cejem/158247.
  • [3] Heger, L. Encyclopedia of Explosives. (in Polish) 1st Ed., Warsaw, Warsaw University of Technology Publishing House, 1979, pp. 159.
  • [4] Okniński, A. HTPB-based Binder Surogates and their Effects on Preliminary Rocket Motor Analyses. Cent. Eur. J. Energ. Mater. 2022, 19(3): 209-230; DOI: 10.22211/cejem/154720.
  • [5] Sutton, G.P.; Biblarz, O. Rocket Propulsion Elements. 8th Ed., New Jersey, John Wiley & Sons, Inc., 2010, pp. 755; ISBN 978-0-470-08024-5.
  • [6] Davenas, A. Solid Rocket Propulsion Technology. Pergamon Press, 1993, pp. 619; ISBN 0-08-040999-7.
  • [7] Florjańczyk, Z.; Penczek, S. Chemistry of Polymers, Basic Synthetic Polymers and Their Applications. (in Polish), Vol. II, Warsaw, Publishing House of the Warsaw University of Technology, 2002, pp. 265-275; ISBN: 83-7207-368-6.
  • [8] Krowicki, K.; Syczewski, M. Solid Rocket Fuels. (in Polish) Warsaw, MON, 1964, pp. 297.
  • [9] Solid and Liquid Fuel Rockets. The European Space Agency, https://www.esa.int/Education/Solid_and_liquid_fuel_rockets4 [Accessed 1 December 2022].
  • [10] Ruffin, A. Study and Development of Throttleable Hybrid Rocket Motors. Ph.D. School STMS, Padova, 2018.
  • [11] Singh, S.; Raveendran, S.; Kshirsagar, D.R.; Gupta, M.; Bhongale, C.J. Studies on Curing of an Aluminized Ammonium Perchlorate Composite Propellant Based on Nitrile Butadiene Rubber Using a Quinol Ether of 1,4-Benzoquinone Dioxime. Cent. Eur. J. Energ. Mater. 2022, 19(1): 18-38; DOI: 10.22211/cejem/147553.
  • [12] Mastrolia, E.J.; Klager, K. Solid Propellants Based on Polybutadiene Binders. Sacramento, Aerojet-General Corp., Propulsion Division, Advances in Chemistry, 1969, pp. 43; ISBN 9780841200890.
  • [13] Crimmins, P.; Cousineau, M.; Rogers, C. The 260 ‒ the Largest Solid Rocket Motor Ever Tested. Gencorp Aerojet, Los Angeles, 1999, pp. 11.
  • [14] Rarata, G.; Surmacz, P. Modern Solid Rocket Propellants. (in Polish) The Papers of the Institute of Aviation 2009, 7: 112-124.
  • [15] Hydroxyl Terminated Polybutadiene Resins and Derivatives ‒ Poly bd and Krasol. Cray Valley, Total, 2022. pp. 44.
  • [16] Gonçalez, V.; Barcia, F.L.; Soares B.G. Composite Materials Based on Modified Epoxy Resin and Carbon Fiber. J. Brazilian Chem. Soc. 2006, 17(6): 1117-1123; DOI: 10.1590/S0103-50532006000600008.
  • [17] Aguiar, M.; Menezes, S.C.; Akcelrud, L. Configurational Double Bond Selectivity in the Epoxidation of Hydroxy-terminated Polybutadiene with m-Chloroperbenzoic Acid. Macromol. Chem. Phys. 1994, 195(12): 3937-3948; DOI: 10.1002/macp.1994.021951219.
  • [18] Zhang, Q. Hydroxyl Terminated Polybutadiene: Chemical Modification and Application of these Modifiers in Propellants and Explosives. Cent. Eur. J. Energ. Mater. 2019, 16(2): 153-193; DOI: 10.22211/cejem/109806.
  • [19] Wang, G. Kinetics of Epoxidation of Hydroxyl-Terminated Polybutadiene with Hydrogen Peroxide under Phase Transfer Catalysis. Ind. Eng. Chem. Res. 2008, 48(3): 1364-1371; DOI: 10.1021/ie800875h.
  • [20] Nikje, M.M.A.; Mozaffari, Z. Chemoselective Epoxidation of Hydroxylterminated Polybutadiene (HTPB) Using in-situ Generated Dimethyl Dioxirane (DMD). Des. Monomers Polym. 2007, 10(1): 67-77; DOI: 10.1163/156855507779763630.
  • [21] Mason, B.P.; Roland, C.M. Solid Propellants. Rubber Chem. Technol. 2019, 92(1): 24; DOI: 10.5254/rct.19.80456.
  • [22] Chai, T. Rheokinetic Analysis on the Curing Process of HTPB-DOA/MDI Binder System. IOP Conf. Ser.: Mater. Sci. Eng. 2016, 137: DOI: 10.1088/1757-899X/137/1/012069.
  • [23] Isocyanates and Isothiocyanates. CAMEO Chemicals, https://cameochemicals.noaa.gov/react/18 [Retrieved 1 Dec. 2022].
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-a89db53e-525b-4cb1-8a9a-c5a47adfd85e
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