[1] Cho BS. and Noh ST. Thermal Properties of Polyurethane Binder with 2‐(Ferrocenylpropyl) Dimethylsilane‐grafted Hydroxyl‐terminated Polybutadiene, Journal of Applied Polymer Science, 121(6), 3560-8, 2011.
[2] Joseph G., Klaubert EC., John SR., Solid Composite Propellants Containing Burning Rate Catalysts. US Pat. 3,386,869, 1968.
[3] Gao JM., Wang L., Yu HJ., Xiao AG., Ding WB. Recent Research Progress in Burning Rate Catalysts. Propellants, Explosives, Pyrotechnics, 36(5), 404-9, 2011.
[4] Gao J., Wang L., Tai YL., Wang J., Huo J., Amin AM., Yu H., Ding W. Study on Poly(errocenylsilane) and its Promotive Effect to Decomposition of Ammonium Perchlorate. Journal of Propulsion and Power, 27(5), 1143-5, 2011.
[5] Pang, W., Li, Y., DeLuca, L.T., Liang, D., Qin, Z., Liu, X., Xu, H. and Fan, X.,. Effect of Metal Nanopowders on the Performance of Solid Rocket Propellants: A Review. Nanomaterials, 11(10), p.2749, 2021.
[6] Elbasuney, S. and Yehia, M., Ferric oxide colloid: A novel nano-catalyst for solid propellants. Journal of Inorganic and Organometallic Polymers and Materials, 30(3), pp.706-713, 2020.
[7] Vara, J.A., Dave, P.N. and Chaturvedi, S., Investigating catalytic properties of nanoferrites for both AP and nano-AP based composite solid propellant. Combustion Science and Technology, 193(13), pp.2290-2304, 2021.
[8] Chen, T., Hu, Y.W., Zhang, C. and Gao, Z.J., Recent progress on transition metal oxides and carbon-supported transition metal oxides as catalysts for thermal decomposition of ammonium perchlorate. Defence Technology, 17(4), pp.1471-1485, 2021.
[9] Ukhin, K.O., Kondrashova, N.B., Valtsifer, V.A., Oshchepkova, T.E., Savastyanova, M.A., Strelnikov, V.N. and Mokrushin, I.G., Metal Oxides/Carbon Black (MOs/CB) Composites and Their Effect on the Thermal Decomposition of Ammonium Perchlorate. Propellants, Explosives, Pyrotechnics, 46(11), pp.1696-1708, 2021.
[10] Gromov, A.A., Slusarsky, K.V., Sergienko, A.V., Popenko, E.M., Dzidziguri, E.L., Larionov, K.B. and Mishakov, I.V., Aluminized Solid Propellants Loaded with Metals and Metal Oxides: Characterization, Thermal Behavior, and Combustion. In Innovative Energetic Materials: Properties, Combustion Performance and Application (pp. 157-182). Springer, Singapore, 2020.
[11] Kretić, D.S., Veljković, I.S., Đunović, A.B. and Veljković, D.Ž., Chelate coordination compounds as a new class of high-energy materials: The case of nitro-bis (acetylacetonato) complexes. Molecules, 26(18), p.5438, 2021.
[12] Amin, B.U., Yu, H., Wang, L., Fahad, S., Nazir, A., Haq, F., Mahmood, S., Uddin, M.A., Shen, D. and Liang, R., Synthesis and Anti-migration Studies of Ferrocene-Based Amides as Burning Rate Catalysts. Journal of Inorganic and Organometallic Polymers and Materials, 31(6), pp.2511-2520, 2021.
[13] Zhang, M., Zhao, F., Wang, Y., Chen, X., Pei, Q., Xu, H., Hao, H., Yang, Y. and Li, H., Evaluation of graphene-ferrocene nanocomposite as multifunctional combustion catalyst in AP-HTPB propellant. Fuel, 302, p.121229, 2021.
[14] Usman, M., Yu, H., Wang, L., Titinchi, S., Khan, A., Nazir, A., Elshaarani, T., Fahad, S. and ul Amin, B.,. Synthesis of poly (2-(methacryloyloxy) ethyl ferrocene carboxylate-co-glycidyl methacrylic acid) s and their anti-migration and burning rate catalytic properties. Journal of Thermal Analysis and Calorimetry, pp.1-18, 2021.
[15] Dubey BL., Nath N., Tripathi A., Tiwari N. Catalysed Combustion of Ammonium Perchlorate, Polystyrene and their Composite Propellants. Indian Journal of Engineering Material and Science, 1, 341-349, 1994.
[16] Grythe KF., Hansen FK. Diffusion Rates and The Role of Diffusion in Solid Propellant Rocket Motor Adhesion. Journal of applied polymer science, 103(3), 1529-38, 2007.
[17] Tang, P., Yang, B., Li, R., Wang, Y., Li, X. and Yang, G.,. Ti3C2 MXene: A reactive combustion catalyst for efficient burning rate control of ammonium perchlorate based solid propellant. Carbon. 2021.
[18] Xu, S., Pang, A.M., Wang, Y., Pan, X.Z., Li, S.W., Li, H.T. and Kong, J., A Review on the Use of Burning Rate Suppressants in AP‐Based Composite Propellants. Propellants, Explosives, Pyrotechnics. 2021.
[19] Yadav, N., Srivastava, P.K. and Varma, M., Recent advances in catalytic combustion of AP-based composite solid propellants. Defence Technology, 17(3), pp.1013-1031. 2021.
[20] Kishore K., Verneker VP., Sunitha MR. Effect of Catalyst Concentration on Burning Rate of Composite Solid Propellants. AIAA Journal, 15(11), 1649-51, 1977.
[21] PittmanC. U. Location of Action of Burning Rate Catalysts in Composite Propellant Combustion. AIAA. Journal, 7(2), 328- 34, 1969.
[22] Dyagileva L.M., Andreev B.Ya. Products of The Thermal Decomposition of Ferrocenes. Trudy Klim. Khim. Tekhnol, 2, 126-27, 1973.
[23] Kebritchi A.Investigation of Ferrocene Polymers as Catalysts for High Energy Composites. Iranian Journal of Research and Development of Polymer Technology, 4(1),45-59, 1395.
[24] Stephens WD., Ashmore CI., Atlantic Research Corp, assignee. Solid Propellant Containing Diferrocenyl Ketone. US Pat. 4,318,760, 1982.
[25] Subramanian K., Synthesis and Characterization of Poly(vinyl ferrocene) Grafted Hydroxyl-Terminated Poly(butadiene): A Propellant Binder with a Built-In Burn-Rate Catalyst.Journal of Polymer Science Part A: Polymer Chemistry, 37(22), 4090-9, 1999.
[26] Mahanta A.K. and Pathak D.D., HTPB-polyurethane: AVersatile Fuel Binder for Composite Solid Propellant,Rijeka, Croatia, Vol. 1, 229-262, 2012.
[27] Vilar WD., Menezes SM., Akcelrud L. Characterization of Hydroxyl-terminated Polybutadiene. Polymer Bulletin, 33(5), 563-70, 1994.
[28] Zhou Q., Jie S. and Li B.G. Preparation of Hydroxyl-Terminated Polybutadiene with High Cis-1, 4 Content.Industrial & Engineering Chemistry Research, 53, 17884-17893, 2014.
[29] Alver Ö., Parlak C. FT-IR, NMR Spectroscopic and Quantum Mechanical Investigations of Two Ferrocene Derivatives. Bulletin of the Chemical Society of Ethiopia, 31(1), 63-74, 2017.
[30] Ghanegharebagh M.,Synthesis of NitratedHydroxyl-terminated Polybutadiene resin (NHTPB)composites, MSc Thesis, Imam Hossein University, February 2018.
[31] Osborn SW., Solid Composite Propellants with Salts of Ferrocene Monosulfonic Acid as Burning Rate Modifiers. US Pat. 3,607,471, 1971.
[32] Ashmore CI., Combs Jr CS., Stephens WD., Solid Propellant Having Incorporated Therein A Ferrocene Combustion Catalyst. US Pat. 4,108,696, 1978.
[33] Teymooriofrad R., Parchebaf M.,Rahimpoor K., Aghaeipoor A.,A Novel Method for Synthesis of 4-Hydroxybutylferrocene as Precursor in Butacene Synthesis,Journal of Energetic Materials, 12 (1), 3-10, 2017
[34] Saravanakumar D., Sengottuvelan N., Narayanan V., Kandaswamy M., Varghese TL. Burning‐rate Enhancement of A High‐energy Rocket Composite Solid Propellant based on Ferrocene‐grafted Hydroxyl‐terminated Polybutadiene Binder. Journal of applied polymer science, 119(5), 2517-24, 2011.
