Статті в журналах з теми "HTPB propellants"
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Kohga, Makoto, Tomoki Naya, and Kayoko Okamoto. "Burning Characteristics of Ammonium-Nitrate-Based Composite Propellants with a Hydroxyl-Terminated Polybutadiene/Polytetrahydrofuran Blend Binder." International Journal of Aerospace Engineering 2012 (2012): 1–9. http://dx.doi.org/10.1155/2012/378483.
Повний текст джерелаLin, Yi-Hsien, Tsung-Mao Yang, Jin-Shuh Li, Kai-Tai Lu, and Tsao-Fa Yeh. "Preliminary Study on Characteristics of NC/HTPB-Based High-Energy Gun Propellants." ChemEngineering 6, no. 5 (October 10, 2022): 80. http://dx.doi.org/10.3390/chemengineering6050080.
Повний текст джерелаDong, Ge, Hengzhi Liu, Lei Deng, Haiyang Yu, Xing Zhou, Xianqiong Tang, and Wei Li. "Study on the interfacial interaction between ammonium perchlorate and hydroxyl-terminated polybutadiene in solid propellants by molecular dynamics simulation." e-Polymers 22, no. 1 (January 1, 2022): 264–75. http://dx.doi.org/10.1515/epoly-2022-0016.
Повний текст джерелаWu, Xinzhou, Jun Li, Hui Ren, and Qingjie Jiao. "Comparative Study on Thermal Response Mechanism of Two Binders during Slow Cook-Off." Polymers 14, no. 17 (September 5, 2022): 3699. http://dx.doi.org/10.3390/polym14173699.
Повний текст джерелаJi, Yongchao, Liang Cao, Zhuo Li, Guoqing Chen, Peng Cao, and Tong Liu. "Numerical Conversion Method for the Dynamic Storage Modulus and Relaxation Modulus of Hydroxy-Terminated Polybutadiene (HTPB) Propellants." Polymers 15, no. 1 (December 20, 2022): 3. http://dx.doi.org/10.3390/polym15010003.
Повний текст джерелаPang, W. Q., F. Q. Zhao, L. T. DeLuca, C. Kappenstein, H. X. Xu, and X. Z. Fan. "Effects of Nano-Sized Al on the Combustion Performance of Fuel Rich Solid Rocket Propellants." Eurasian Chemico-Technological Journal 18, no. 3 (November 5, 2016): 197. http://dx.doi.org/10.18321/ectj425.
Повний текст джерелаDewi, Wiwiek Utami. "EVALUASI KINETIKA DEKOMPOSISI TERMAL PROPELAN KOMPOSIT AP/HTPB DENGAN METODE KISSINGER, FLYNN WALL OZAWA DAN COATS - REDFREN." Jurnal Teknologi Dirgantara 15, no. 2 (February 27, 2018): 115. http://dx.doi.org/10.30536/j.jtd.2017.v0.a2635.
Повний текст джерелаWang, Qizhou, Guang Wang, Zhejun Wang, Hongfu Qiang, Xueren Wang, and Shudi Pei. "Strain-rate correlation of biaxial tension and compression mechanical properties of HTPB and NEPE propellants." AIP Advances 12, no. 5 (May 1, 2022): 055005. http://dx.doi.org/10.1063/5.0083205.
Повний текст джерелаChaturvedi, Shalini, and Pragnesh N. Dave. "Solid propellants: AP/HTPB composite propellants." Arabian Journal of Chemistry 12, no. 8 (December 2019): 2061–68. http://dx.doi.org/10.1016/j.arabjc.2014.12.033.
Повний текст джерелаXie, Zhi Min, Si Chi Chen, and You Shan Wang. "Relaxation Properties of the Solid Propellant Based on Hydroxyl-Terminated Polybutadiene." Advanced Materials Research 989-994 (July 2014): 172–76. http://dx.doi.org/10.4028/www.scientific.net/amr.989-994.172.
Повний текст джерелаAbd-Elghany, Mohamed, Thomas M. Klapötke, and Ahmed Elbeih. "Environmentally safe (chlorine-free): new green propellant formulation based on 2,2,2-trinitroethyl-formate and HTPB." RSC Advances 8, no. 21 (2018): 11771–77. http://dx.doi.org/10.1039/c8ra01515e.
Повний текст джерелаHoque, Ehtasimul, Chandra Shekhar Pant, and Sushanta Das. "Study on Friction Sensitivity of Passive and Active Binder based Composite Solid Propellants and Correlation with Burning Rate." Defence Science Journal 70, no. 2 (March 9, 2020): 159–65. http://dx.doi.org/10.14429/dsj.70.14802.
Повний текст джерелаRosita, Geni. "RETIKULASI HIDROXYL TERMINATED POLUBUTADIENE (HTPB) MANDIRI DENGAN TOLUENE DIISOCIANATE (TDI) MEMBENTUK POLIURETAN SEBAGAI FUEL BINDER PROPELAN." Jurnal Teknologi Dirgantara 14, no. 1 (July 22, 2016): 51. http://dx.doi.org/10.30536/j.jtd.2016.v14.a2567.
Повний текст джерелаRosita, Geni. "RETIKULASI HIDROXYL TERMINATED POLUBUTADIENE (HTPB) MANDIRI DENGAN TOLUENE DIISOCIANATE (TDI) MEMBENTUK POLIURETAN SEBAGAI FUEL BINDER PROPELAN." Jurnal Teknologi Dirgantara 14, no. 1 (March 19, 2018): 51. http://dx.doi.org/10.30536/j.jtd.2016.v14.a2947.
Повний текст джерелаVorozhtsov, Alexander, Marat Lerner, Nikolay Rodkevich, Sergei Sokolov, Elizaveta Perchatkina, and Christian Paravan. "Preparation and Characterization of Al/HTPB Composite for High Energetic Materials." Nanomaterials 10, no. 11 (November 8, 2020): 2222. http://dx.doi.org/10.3390/nano10112222.
Повний текст джерелаTang, Yuqing, Hanyu Deng, Tenghui Liao, and Yingjian Qi. "Research on the vacuum aging performance of HTPB propellant based on the DSC method." Journal of Physics: Conference Series 2403, no. 1 (December 1, 2022): 012013. http://dx.doi.org/10.1088/1742-6596/2403/1/012013.
Повний текст джерелаvan der Heijden, A. E. D. M., H. L. J. Keizers, and W. H. M. Veltmans. "HNF/HTPB BASED COMPOSITE PROPELLANTS." International Journal of Energetic Materials and Chemical Propulsion 5, no. 1-6 (2002): 587–96. http://dx.doi.org/10.1615/intjenergeticmaterialschemprop.v5.i1-6.610.
Повний текст джерелаBekhouche, Slimane, and Yun Jun Luo. "Research of Formulation and Processing of Hydroxyl-Terminated Polybutadiene (HTPB) Propellants." Advanced Materials Research 1030-1032 (September 2014): 155–60. http://dx.doi.org/10.4028/www.scientific.net/amr.1030-1032.155.
Повний текст джерелаTraissac, Y., J. Ninous, R. Neviere, and J. Pouyet. "Mechanical Behavior of a Solid Composite Propellant during Motor Ignition." Rubber Chemistry and Technology 68, no. 1 (March 1, 1995): 146–57. http://dx.doi.org/10.5254/1.3538726.
Повний текст джерелаYang, Yi, Xinjie Yu, Jun Wang, and Yaxue Wang. "Effect of the Dispersibility of Nano-CuO Catalyst on Heat Releasing of AP/HTPB Propellant." Journal of Nanomaterials 2011 (2011): 1–5. http://dx.doi.org/10.1155/2011/180896.
Повний текст джерелаYao, Er Gang, Feng Qi Zhao, Si Yu Xu, Rong Zu Hu, Hui Xiang Xu, and Hai Xia Hao. "Combustion Characteristics of Composite Solid Propellants Containing Different Coated Aluminum Nanopowders." Advanced Materials Research 924 (April 2014): 200–211. http://dx.doi.org/10.4028/www.scientific.net/amr.924.200.
Повний текст джерелаQin, Zhao, Jiang Wu, Rui Qi Shen, Ying Hua Ye, and Li Zhi Wu. "Laser-Controlled Combustion of Solid Propellant." Advanced Materials Research 884-885 (January 2014): 87–90. http://dx.doi.org/10.4028/www.scientific.net/amr.884-885.87.
Повний текст джерелаMukhtar, Amir, Habib Nasir, and Hizba Waheed. "Pressure-Time Study of Slow Burning Rate Ap/HTPB Based Composite Propellant by Using Closed Vessel Test (CVT)." Key Engineering Materials 778 (September 2018): 268–74. http://dx.doi.org/10.4028/www.scientific.net/kem.778.268.
Повний текст джерелаLin, Guomin, Yixue Chang, Yu Chen, Wei Zhang, Yanchun Ye, Yanwen Guo, and Shaohua Jin. "Synthesis of a Series of Dual-Functional Chelated Titanate Bonding Agents and Their Application Performances in Composite Solid Propellants." Molecules 25, no. 22 (November 16, 2020): 5353. http://dx.doi.org/10.3390/molecules25225353.
Повний текст джерелаDostanic, Jasmina, Gordana Uscumlic, Tatjana Volkov-Husovic, Radmila Jancic-Heinemann, and Dusan Mijin. "The use of image analysis for the study of interfacial bonding in solid composite propellant." Journal of the Serbian Chemical Society 72, no. 10 (2007): 1023–30. http://dx.doi.org/10.2298/jsc0710023d.
Повний текст джерелаYogeshkumar, Velari, Nikunj Rathi, and P. A. Ramakrishna. "Solid Fuel rich Propellant Development for use in a Ramjet to Propel an Artillery Shell." Defence Science Journal 70, no. 3 (April 24, 2020): 329–35. http://dx.doi.org/10.14429/dsj.70.15061.
Повний текст джерелаKorobeinichev, Oleg P., and Alexander A. Paletsky. "Flame structure of ADN/HTPB composite propellants." Combustion and Flame 127, no. 3 (November 2001): 2059–65. http://dx.doi.org/10.1016/s0010-2180(01)00308-x.
Повний текст джерелаCui, Huiru, Xuan Lv, Yurong Xu, Zhiwen Zhong, Zixiang Zhou, and Weili Ma. "A Step-by-Step Equivalent Microprediction Method for the Mechanical Properties of Composite Solid Propellants considering Dewetting Damage." International Journal of Aerospace Engineering 2022 (February 14, 2022): 1–12. http://dx.doi.org/10.1155/2022/2427463.
Повний текст джерелаAjaz, A. G. "Hydroxyl-Terminated Polybutadiene Telechelic Polymer (HTPB): Binder for Solid Rocket Propellants." Rubber Chemistry and Technology 68, no. 3 (July 1, 1995): 481–506. http://dx.doi.org/10.5254/1.3538752.
Повний текст джерелаKim, Ki-Hong, Chang-Kee Kim, Ji-Chang Yoo, and Jack J. Yoh. "Test-Based Thermal Decomposition Simulation of AP/HTPB and AP/HTPE Propellants." Journal of Propulsion and Power 27, no. 4 (July 2011): 822–27. http://dx.doi.org/10.2514/1.b34099.
Повний текст джерелаAziz, Amir, and Wan Khairuddin bin Wan Ali. "A Study of Basic Aluminized Propellants Characteristics." Applied Mechanics and Materials 110-116 (October 2011): 1321–27. http://dx.doi.org/10.4028/www.scientific.net/amm.110-116.1321.
Повний текст джерелаJabez, I. Kingstone Lesley, Urmila Das, R. Manivannan, and Sarat Babu Anne. "Influence of HTPB prepolymer on achieved properties of composite solid propellant." High Performance Polymers 31, no. 9-10 (February 26, 2019): 1162–72. http://dx.doi.org/10.1177/0954008319830468.
Повний текст джерелаBogusz, Rafał, Paulina Magnuszewska, and Bogdan Florczak. "STUDIES OF HIGH EXPLOSIVES IMPACT ON REDUCTION OF HCL IN HETEROGENEOUS SOLID ROCKET PROPELLANTS." PROBLEMY TECHNIKI UZBROJENIA, no. 3 (December 1, 2017): 29–45. http://dx.doi.org/10.5604/01.3001.0010.6308.
Повний текст джерелаRuntu, Khevinadya Ramadhani, Wahyu Sri Setiani, and Mala Utami. "Application Energetic Materials for Solid Composite Propellant to Support Defense Rocket Development." International Journal of Social Science Research and Review 6, no. 1 (January 6, 2023): 153–59. http://dx.doi.org/10.47814/ijssrr.v6i1.756.
Повний текст джерелаBaker, P. J., A. M. Mellor, and C. S. Coffey. "Critical impact initiation energies for three HTPB propellants." Journal of Propulsion and Power 8, no. 3 (May 1992): 578–85. http://dx.doi.org/10.2514/3.23517.
Повний текст джерелаVenugopal, S. "Combustion experiments of HTPB/RFNA mixed hybrid propellants." Indian Journal of Science and Technology 4, no. 10 (October 20, 2011): 1267–73. http://dx.doi.org/10.17485/ijst/2011/v4i10.8.
Повний текст джерелаGupta, D. C., S. S. Deo, D. V. Wast, S. S. Raomore, and D. H. Gholap. "HTPB-based polyurethanes for inhibition of composite propellants." Journal of Applied Polymer Science 55, no. 8 (February 22, 1995): 1151–55. http://dx.doi.org/10.1002/app.1995.070550801.
Повний текст джерелаPRASUŁA, Piotr, Beata SZTEJTER, Piotr KASPRZAK, and Michał CHMIELAREK. "INCREASING THE ENERGY OF alpha, omega - DIHYDROXYPOLIBUTADIENE (HTPB) USED IN SOLID HETEROGENEOUS ROCKET PROPELLANT." PROBLEMY TECHNIKI UZBROJENIA 161, no. 3 (November 29, 2022): 37–59. http://dx.doi.org/10.5604/01.3001.0016.1154.
Повний текст джерелаCauty, Franck, Yves Fabignon, and Charles Erades. "NEW ACTIVE BINDER-BASED PROPELLANTS: A COMPARISON WITH CLASSICAL COMPOSITE AP/HTPB PROPELLANTS." International Journal of Energetic Materials and Chemical Propulsion 12, no. 1 (2013): 1–13. http://dx.doi.org/10.1615/intjenergeticmaterialschemprop.2013005271.
Повний текст джерелаPinalia, Anita, Bayu Prianto, Henny Setyaningsih, Prawita Dhewi, and Ratnawati Ratnawati. "Design of Propellant Composite Thermodynamic Properties Using Rocket Propulsion Analysis (RPA) Software." Reaktor 22, no. 1 (July 12, 2022): 1–6. http://dx.doi.org/10.14710/reaktor.22.1.1-6.
Повний текст джерелаAraujo, Luis, and Octavia Frota. "ON THERMOCHEMICAL CHARACTERISTICS OF AP/NSAN/HTPB COMPOSITE PROPELLANTS." International Journal of Energetic Materials and Chemical Propulsion 4, no. 1-6 (1997): 118–28. http://dx.doi.org/10.1615/intjenergeticmaterialschemprop.v4.i1-6.140.
Повний текст джерелаNaseem, Hamza, Jyothsna Yerra, H. Murthy, and P. A. Ramakrishna. "Ageing studies on AP/HTPB based composites solid propellants." Energetic Materials Frontiers 2, no. 2 (June 2021): 111–24. http://dx.doi.org/10.1016/j.enmf.2021.02.001.
Повний текст джерелаXu, Hui-Xiang, Feng-Qi Zhao, Wei-Qiang Pang, Hong-Wei Guo, Zhi-Hua Sun, and Xue-Zhong Fan. "Application Characteristics of Ammonium Dinitramide to HTPB Composite Propellants." Asian Journal of Chemistry 26, no. 13 (2014): 3995–99. http://dx.doi.org/10.14233/ajchem.2014.16516.
Повний текст джерелаErişken, Cevat, Ahmet Göçmez, Ülkü Yilmazer, Fikret Pekel, and Saim Özkar. "Modeling and rheology of HTPB based composite solid propellants." Polymer Composites 19, no. 4 (August 1998): 463–72. http://dx.doi.org/10.1002/pc.10121.
Повний текст джерелаDésilets, Sylvain, and Sébastien Côté. "Chemical Bond Between Stabilizers and HTPB Binders in Propellants." Propellants, Explosives, Pyrotechnics 25, no. 4 (September 2000): 186–90. http://dx.doi.org/10.1002/1521-4087(200009)25:4<186::aid-prep186>3.0.co;2-b.
Повний текст джерелаPatil, M. S., and Haridwar Singh. "Ballistic and mechanical properties of HTPB based composite propellants." Journal of Hazardous Materials 19, no. 3 (January 1988): 271–78. http://dx.doi.org/10.1016/0304-3894(88)80026-8.
Повний текст джерелаManjari, R., V. C. Joseph, L. P. Pandureng, and T. Sriram. "Structure-property relationship of HTPB-based propellants. I. Effect of hydroxyl value of HTPB resin." Journal of Applied Polymer Science 48, no. 2 (April 10, 1993): 271–78. http://dx.doi.org/10.1002/app.1993.070480211.
Повний текст джерелаLee, Sunyoung, Taeha Ryu, Myungpyo Hong, and Hyoungjin Lee. "Study on the Enhancement of Burning Rate of HTPB/AP Solid Propellants." Journal of the Korean Society of Propulsion Engineers 21, no. 4 (August 1, 2017): 21–27. http://dx.doi.org/10.6108/kspe.2017.21.4.021.
Повний текст джерелаKrishnan, S., and R. Jeenu. "Combustion characteristics of AP/HTPB propellants with burning rate modifiers." Journal of Propulsion and Power 8, no. 4 (July 1992): 748–55. http://dx.doi.org/10.2514/3.23545.
Повний текст джерелаHickman, S. R., and M. Q. Brewster. "Oscillatory Combustion of Fine-AP/HTPB Propellants: Disproportionate Pyrolysis Response." Journal of Propulsion and Power 16, no. 5 (September 2000): 867–73. http://dx.doi.org/10.2514/2.5652.
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