KAJIAN PROGRAM PENINGKATAN KINERJA PROPELAN KOMPOSIT BERBASIS AP/HTPB/AL

Heri Budi Wibowo

Abstract

Kajian strategi litbang dalam meningkatkan kinerja propelan komposit berbasis AP/HTPB/Al dilakukan dalam rangka mencapai teknologi propelan yang setara dengan negara maju dalam penguasaan teknologi roket sipil, khususnya untuk roket Sonda dan roket Pengorbit Satelit di LAPAN. Kajian dilakukan dengan melakukan review terhadap capaian proplelan saat ini, analisis penyebab-penyebabnya, dan penyusunan strategi untuk mengatasinya. Hasil kajian menunjukkan bahwa diperlukan organisasi, tahapan litbang dan pengelolaan SDM yang sistematis, serta tahapan pencapaian teknologi yang perlu dilakukan. Keterbatasan bahan baku propelan merupakan masalah utama dalam pengembangan propelan di Indonesia. Peningkatan kinerja propelan dapat dilakukan dengan meningkatkan solid loading density dan penambahan bahan energetik tinggi.

Keywords

propelan komposit, kinerja propelan, roket sonda

Full Text:

PDF

References

Abdullah, M., Gholamian, F., and Zarei, A. R., 2014. Investigation of Composite Solid Propellants Based on Nitrated Hydroxyl-Terminated Polybutadiene Binder. Journal of Propulsion and Power, 30(3), 862–864. https://doi.org/10.2514/1.B35117

Abusaidi, H., Ghaieni, H. R., & Ghorbani, M., 2017. Influences of NCO/OH and triol/diol ratios on the mechanical properties of nitro-HTPB based polyurethane elastomers. Iranian Journal of Chemistry and Chemical Engineering, 36(5), 55–63.

Abusaidi, H., Ghorbani, M., & Ghaieni, H. R., 2017. Development of Composite Solid Propellant Based on Nitro Functionalized Hydroxyl-Terminated Polybutadiene. Propellants, Explosives, Pyrotechnics, 42(6), 671–675. https://doi.org/10.1002/prep.201600120

Agrawal, J. P., 2010. High Energy Materials: Propellants, Explosives and Pyrotechnics. Wiley-VCH Verlag GmbH & Co.

Ashrafi, M., Fakhraian, H., and Dehnavi, M. A., 2016. Synthesis , Characterization and Properties of Nitropolybutadiene as Energetic Plasticizer for NHTPB Binder. Propellants, Explosives, Pyrotechnics, 1–8. https://doi.org/10.1002/prep.201600057

Badgujar, D.M., Talawar, M.B., Asthana, S.N., and Mahulikar, P.P., 2008. Advances in Science and Technology of Modern Energetic Materials: An Overview, Journal of Hazardous Materials, 151, pp. 289–305.

Betzler, F. M., Hartdegen, V. A., Klapötke, T. M., and Sproll, S. M., 2016. A new energetic binder: Glycidyl nitramine polymer. Central European Journal of Energetic Materials, 13(2), 289–300. https://doi.org/10.22211/cejem/64984

Colclough, M. E., Desai, H., Millar, R. W., Paul, N. C., Stewart, M. J., and Golding, P., 1993. Energetic Polymers as Binders in Composite Propellants and Explosives. Polymers for Advanced Technologies, 5(September), 554–560.

Colclough, M. E., and Paul, N. C., 1996. Nitrated Hydroxy-Terminated Polybutadiene : Synthesis and Properties. In A. L (Ed.), ACS Symposium Series (pp. 97–103). Washington, DC: American Chemical Society. https://doi.org/10.1021/bk-1996-0623.ch010

Chen, C.Y., Wang, X.F., Gao, L.L. and Zheng Y.F., 2013. Effect of HTPB with different molecular weights on curing kinetics of HTPB/TDI System, Chinese Journal of Energetic Materials, 21(6), pp. 771-776.

Cuihua, L., Tao, L., Xiaoxue, Z., Jianhong, L., Aimin, P. and Xuhui. C, 2016. Curing reaction bentween HTPB and IPDI, Journal of Shenzhen University Science and Engineering, 33(5), pp. 452-456.

Florczak, B., Bogusz, R., Skupiński, W., Chmielarek, M. and Dzik, A., 2015. Study of the Effect of Nitrated Hydroxyl-terminated Polybutadiene (NHTPB) on the Properties of Heterogeneous Rocket Propellants Central European Journal of Energetic Materials 12(4) 841-854.

Gupta, B. ., Kumar, V., and Shivhare, N., 2014. Rheological Studies on Virgin, Plasticized and Solid Filled HTPB Binder System. Global Journal of Advanced Engineering Technologies and Sciences, 1(2), 41–48. Retrieved from http://www.gjaets.com

Hartaya,K., 2015. Penyempurnaan Proses Pembuatan Propelan Komposit Lapan Berdasar Hasil Penelitian dari India, Jurnal Teknologi Dirgantara Vol. 13 No. 2 Desember 2015, pp. 121-130

Krishnan, G., Ayyaswamy, K., and Nayak, S.K., 2012. Hydroxy Terminated polybutadiene: chemical modifications and application J. Macro. Sci. Part A, 50(1), pp. 128-138.

Komarov, V. F., and Shandakov, V. A. 1999. Solid Fuels, their properties, and applications. Combustion, Explosion, and Shock Waves, 35(2), 2–6. https://doi.org/https://doi.org/10.1007/BF02674426

Kshirsagar D.R., Jain, S., Bhandarkar, S., Vemuri, M., and Mehilal, 2017. Studies on the Effect of Nano-MnO2 in HTPB-based Composite Propellant Formulations, Cent. Eur. J. Energ. Mater., 14(3), pp. 589-604.

Kumari A, Kurva R, Jain S and Bhattacharya B 2009 Size and Shape of Ammonium Perchlorate and their Influence on Properties of Composite Propellant Defence Science Journal 59(3) 294-299.

Kumari, A., Kurva, R., Jain, S. and Bhattacharya, B., 2015. Evaluation of nanoalumunium in Composite Propellant Formulation Using Bicurative System, Journal of Propulsion and Power, 31(1), pp. 393-399.

Kumari, A., Maurya, M., Jain, S., and Bhattacharya, B., 2017. Nano-Ammoinum Perchlorate: Preparation, Characterization, and Evaluation in Composite Propellant Formulation, Journal of Energetic Materials, 31(3), pp. 115-119.

Loekman, S., Pengembangan Propelan Komposit, 1998, Majalah LAPAN No2, LAPAN.

Priyanto, B., Pinalia, A., and Puspitasari, R.R., 2015. The Effect of Spray Gas Flow Rate and Concentration on Modification Ammonium Perchlorate Using Spray Drying: Advances in Science and Technology of Indonesian Aircraft, Rocket, and Satellite, Indonesia Book Project, pp. 22-31.

Rahman, A., Chin, J. and Cheah, K.H., 2018. Prilling and Coating of And Solid Green Propellant in Toluene Mixture Using Ultrasound Sonication, Aerospace, 5(1), pp. 29-35.

Ramezani, A. and Rothe, H., 2017. Simulation Based Early Prediction of Rocket, Artillery, and Mortar Trajectories and Real Time Optimization for Counter RAM Systems Mathematical Problems in Engineering, 12, pp. 1-8.

Ramesh, K., Jawalkar, S. N., Sachdeva, S., Mehilal, and Bhattacharya, B., 2012. Development of a Composite Propellant Formulation with a High Performance Index Using a Pressure Casting Technique. Central European Journal of Energetic Materials, 9(1), 49–58.

Restasari, A., Hartaya, K., Ardianingsih, R. and Abdillah, L.H., 2015. Effects of Toluene Diisocyanate`s Chemical Structure on Polyurethane`s Viscosity and Mechanical Properties for Propellant, Proceedings ISAST III-2015, 2015, pp. 59-67.

Salgado, M.C., Belderrain, M.S.N., and Devezas, T.C., 2018. Space Propulsion: a Survey Study about Current and Future Technologies, J. aerosp. Technol. Manag., 10, pp. 1-10.

Sariak, G., 2017. Between a Rocket and a Hard Place: Militar Space Technology and Stability in International Relations, The internastional Journal of Space Polytics & Policy, 15(1), pp. 51-64.

Schulze, M.C. and Chavez, D.E., 2016, Synthesis and Characterization of Energetic Plasctcizer AMDNNM, Journal of Energetic Materials, 34(2), pp. 129-137.

Shokry, S.A., El-Morsi, A.K., Sabaa, M.S., Mohamed, R.R. and El Sorogy, H.E., 2015. Synthesis and characterization of polyurethane based on hydroxyl terminated polybutadiene and reinforced by carbon nanotubes, Egyptian Journal of Petroleum, 24(2), pp. 113–232.

Shekhar, C., Pant, M.S., Santosh, S., Banerjee, P.K., Khanna, 2013. Single Step Synthesis of Nitro-Functionalized Hydroxyl-Terminated Polybutadiene, Propellants Explos. Pyrotech., 38, pp. 748-753.

Trache, D., Klapotke, T.M., Maiz, L., Abd-Elghany, M. and DeLuca, L.T., 2017. Green Chamistry, 20, pp. 4711-4736.

Timnat, Y.M., 1987. Advanced Chemical Rocket Propulsion, Academic Press, pp. 132-135

Wibowo, H.B., 2015. Peningkatan Sifat Mekanik Propelan Mandiri Berbasis Pengaruh Bilangan OH terhadap Kinerja Propelan: Teknologi Roket Sonda Indonesia 2015, Penerbit Indonesia Book Project, pp. 273-290.

Wibowo, H.B., 2015. Pengembangan Propelan Mandiri untuk Roket Komposit. Prosiding JASAKIAI 21 November 2013, pp. 157-162.

Wibowo, H.B., 2016. Kontrol Kualitas Bahan Baku Propelan, Penerbit Indonesia Book Project, pp. 134-139.

Wibowo, H.B., 2016. Polimer HTPB Pengembangan Binder Propelan Komposit Di Indonesia, Penerbit Indonesia Book Project, pp. 120-129.

Wibowo, H.B., 2017, Teknologi PropelanUntuk Penguasaan Teknologi Roket, Bahan Orasi Profesor Riset, LIPI, pp. 78-80

Zhou, Q., Jie, S. and Li, B.G., 2014. Preparation of Hydroxyl Terminated Polybutadiene, Ind. Eng. Chem. Res., 53(46), pp. 17884–17893.

DOI: http://dx.doi.org/10.30536/j.jtd.2018.v16.a3002

Refbacks

  • There are currently no refbacks.