Hydroxyl Terminated Natural Rubber (HTNR) as a Binder in Solid Rocket Propellant

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Controlled degradation of deproteinized natural rubber by oxidative method using cobaltous leading to the formation of telechelic liquid natural rubber (TLNR) has been the subject of study in the current work. Hydroxyl-terminated natural rubber (HTNR) having number-average molecular weights (Mn) below 10,000 gmol-1 were synthesized at temperatures 60°C using Cobalt bis (acetyl acetonate) (Co) in the presence of ethanol and Sodium borohydride. The HTNR were characterized structurally by using Fourier Transform Infrared (FTIR), Gel Permeation Chromatography (GPC) and Nuclear Magnetic Resonance (NMR) spectroscopy. From the FTIR and GPC analysis, one hour reaction showed the lowest Mn around 6691 gmol-1 comparable to Hydroxyl terminated polybutadiene (HTPB) which were 7708 gmol-1. As the reaction time increases the Mn also increase up to 8 hours of reaction. FTIR indicated that the synthesized HTNR contained hydroxyl end groups. The study showed the optimum percentage of Cobalt bis (acetyl acetonate) is 5% which produce the lowest molecular weight. Next, the HTNR underwent crosslinking reaction with isophore diisocyanate (IPDI). Then, metal fuel (aluminium powder, Al), oxidizer (ammonium perchlorate, AP) and HTNR were mixed together and went through compression process to produce solid rocket propellant. Burning rate obtained from HTNR samples were 2.78 mms-1 which were equivalent to HTPB samples which is 2.94 mms-1.

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174-178

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November 2014

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© 2015 Trans Tech Publications Ltd. All Rights Reserved

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[1] A. Saetung, A. Rungvichaniwat, I. Campistron, P. Klinpituksa, A. Laguerre, P. Phinyocheep, and J.F. Pilard, Controlled Degradation of Natural Rubber and Modification of the Obtained Telechelic Oligoisoprenes: Preliminary Study of Their Potentiality as Polyurethane Foam Precursors, J. of Applied Polymer Science. 117 (2010).

DOI: 10.1002/app.31907

Google Scholar

[2] K. A. Dubkov, S. V. Semikolenov, D. E. Babushkin, L.G. Echevskaya, M.A. Matsko, D. P. Ivanov, v. A. Zakharov, V. N. Parmon, and G. I. Panov, New Reaction for the Preparation of Liquid Rubber, Jounal of Polymer Science: Part A: Polymer Chemistry. 44 (2006).

DOI: 10.1002/pola.21353

Google Scholar

[3] F. Cataldo, Preparation and Evaluation of Thermally Depolymerized Natural Rubber in Rubber Compound Formulations, Progress in Rubber, Plastics and Recycling Technology. 22 (2006) 147-163.

DOI: 10.1177/147776060602200301

Google Scholar

[4] T. Ravindran, N. Gopinathan, M.R. and J. D. Francis, A novel method for the preparation of hydroxyl terminated liquid natural rubber, Macromol. Chem. Rapid Commun. 7 (1986) 159-163.

Google Scholar

[5] S.K. Gupta, M.R. Kurup, E. Devadoss, R.M. Muthiah, and S. Thomas, Development and Evaluation of a Novel Binder Based on Natural Rubber and High-Energy Polyurethane/Composite Propellants, Journal of Applied Polymer Science. 30 (1985) 1095-1112.

DOI: 10.1002/app.1985.070300317

Google Scholar

[6] H. Mohd Nor, and J.R. Ebdon, Telechelic Liquid Natural Rubber: A Review, Prog. Polymer Science. 23 (1998) 143-177.

DOI: 10.1016/s0079-6700(97)00028-2

Google Scholar

[7] V.N. Krishnamurthy, and S. Thomas, ISRO Polyol – The Versatile Binder for Launch Vehicles and Missiles, Defence Science Journal. 37(1) (1987) 29-37.

DOI: 10.14429/dsj.37.5889

Google Scholar

[8] H. Maruizumi, K. Kosaka, S. Suzuki, D. Fukuma and A. Yamamoto, Development of HTPB Binder for Solid Propellants, AIAA/SAE/ASME/ASEE 24th Joint Propulsion Conference. 11-13 July 1988. Boston, Massachusetts, 1-5.

DOI: 10.2514/6.1988-3352

Google Scholar

[9] R.M. Muthiah, R. Manjari, and V.N. Krishnamurthy, Rheology of HTPB Propellant: Effect of Mixing Speed and Mixing Time, Defence Science Journal. 43(2) (1993) 167-172.

DOI: 10.14429/dsj.43.4328

Google Scholar

[10] S. Thomas, T.L. Varghese, S.K. Gupta, T.S. Ram, and V.N. Krishnamurthy, Natural Rubber-Based Fuel Rich Propellant for Ramjet Rocket, Defence Science Journal. 42(3) (1992) 141-146.

DOI: 10.14429/dsj.42.4373

Google Scholar

[11] Y. Tanaka, T. Sakaki, A. Kawasaki, M. Hayashi, E. Kanamaru, and K. Shibata, European Patent 0 702 029 B1. (1995).

Google Scholar