Добірка наукової літератури з теми "HTPB propellants"
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Статті в журналах з теми "HTPB propellants"
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 джерелаДисертації з теми "HTPB propellants"
Rossetti, Edoardo. "Evaluation of the ballistic properties of a solid propellant from its granulometric composition." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2021.
Знайти повний текст джерелаSmyth, Daniel A. "Modeling Solid Propellant Ignition Events." BYU ScholarsArchive, 2011. https://scholarsarchive.byu.edu/etd/3125.
Повний текст джерелаStyborski, Jeremy A. "Effects of aluminum and iron nanoparticle additives on composite AP/HTPB solid propellant regression rate." Thesis, Rensselaer Polytechnic Institute, 2014. http://pqdtopen.proquest.com/#viewpdf?dispub=1561975.
Повний текст джерелаThis project was started in the interest of supplementing existing data on additives to composite solid propellants. The study on the addition of iron and aluminum nanoparticles to composite AP/HTPB propellants was conducted at the Combustion and Energy Systems Laboratory at RPI in the new strand-burner experiment setup. For this study, a large literature review was conducted on history of solid propellant combustion modeling and the empirical results of tests on binders, plasticizers, AP particle size, and additives.
The study focused on the addition of nano-scale aluminum and iron in small concentrations to AP/HTPB solid propellants with an average AP particle size of 200 microns. Replacing 1% of the propellant's AP with 40-60 nm aluminum particles produced no change in combustive behavior. The addition of 1% 60-80 nm iron particles produced a significant increase in burn rate, although the increase was lesser at higher pressures. These results are summarized in Table 2. The increase in the burn rate at all pressures due to the addition of iron nanoparticles warranted further study on the effect of concentration of iron. Tests conducted at 10 atm showed that the mean regression rate varied with iron concentration, peaking at 1% and 3%. Regardless of the iron concentration, the regression rate was higher than the baseline AP/HTPB propellants. These results are summarized in Table 3.
Ruffilli, Davide. "Simulation of the casting process of an Al-AP-HTPB propellant with an open source solver." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2021.
Знайти повний текст джерелаTanner, Matthew Wilder. "Multidimensional Modeling of Solid Propellant Burning Rates and Aluminum Agglomeration and One-Dimensional Modeling of RDX/GAP and AP/HTPB." Diss., CLICK HERE for online access, 2008. http://contentdm.lib.byu.edu/ETD/image/etd2706.pdf.
Повний текст джерелаGross, Matthew L. "Two-Dimensional Modeling of AP/HTPB Utilizing a Vorticity Formulation and One-Dimensional Modeling of AP and ADN." Diss., CLICK HERE for online access, 2007. http://contentdm.lib.byu.edu/ETD/image/etd2077.pdf.
Повний текст джерелаMateille, Pierre. "Analyse multi-échelle des phénomènes d'endommagement d'un matériau composite de type propergol, soumis à un impact de faible intensité." Phd thesis, Université Montpellier II - Sciences et Techniques du Languedoc, 2010. http://tel.archives-ouvertes.fr/tel-00797604.
Повний текст джерелаSekkar, V. "Studies On HTPB Based Copolyurethanes As Solid Propellant Binders : Characterization And Modeling Of Network Parameters." Thesis, 1996. http://etd.iisc.ernet.in/handle/2005/1569.
Повний текст джерелаStephens, Matthew. "TAILORING THE PLATEAU BURNING RATES OF COMPOSITE PROPELLANTS BY THE USE OF NANOSCALE ADDITIVES." 2009. http://hdl.handle.net/1969.1/ETD-TAMU-2009-05-418.
Повний текст джерелаZHU, JUN-JI, and 朱俊吉. "Aging studies on HTPB/Ap/Al composite propellant." Thesis, 1990. http://ndltd.ncl.edu.tw/handle/02356588642215623369.
Повний текст джерелаЧастини книг з теми "HTPB propellants"
Zhao, Xitong, Xiaolong Fu, Zhengming Gao, Liping Jiang, Jizhen Li, and Xuezhong Fan. "Molecular Dynamics Study on Aging Mechanism of HTPB Propellants." In Springer Proceedings in Physics, 595–609. Singapore: Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-1774-5_44.
Повний текст джерелаDubey, Vanchhit Kumar, Sri Nithya Mahottamananda, Afreen Abdul Khaleel, P. N. Kadiresh, and M. Thirumurugan. "Mechanical Characteristics of Paraffin Wax, Beeswax and HTPB as Rocket Propellant—A Comparative Study." In Advances in Design and Thermal Systems, 243–52. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-33-6428-8_18.
Повний текст джерелаRocha, Roberta Jachura. "Accelerated Aging Tests of HTPB-Based Propellants." In Energetic Materials Research, Applications, and New Technologies, 246–71. IGI Global, 2018. http://dx.doi.org/10.4018/978-1-5225-2903-3.ch012.
Повний текст джерела"Combustion Characteristics of Aluminized HTPB/AP Propellants in Acceleration Fields." In Solid Propellant Chemistry, Combustion, and Motor Interior Ballistics, 907–20. Reston ,VA: American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/5.9781600866562.0907.0920.
Повний текст джерелаAlmeida, Luis Eduardo Nunes, Aureomar F. Martins, Susane R. Gomes, and Flavio A. L. Cunha. "Thermal Decomposition Kinetics Studies of HTPB/Al/AP Solid Propellants Formulated With Iron Oxide Burning Rate Catalyst in Nano and Micro Scale." In Energetic Materials Research, Applications, and New Technologies, 211–33. IGI Global, 2018. http://dx.doi.org/10.4018/978-1-5225-2903-3.ch010.
Повний текст джерелаK., Abhay, and Devendra D. "HTPB-Polyurethane: A Versatile Fuel Binder for Composite Solid Propellant." In Polyurethane. InTech, 2012. http://dx.doi.org/10.5772/47995.
Повний текст джерелаB. Goncalves, R. F., J. A. F. F. Rocco, and K. Ih. "Thermal Decomposition Kinetics of Aged Solid Propellant Based on Ammonium Perchlorate – AP/HTPB Binder." In Applications of Calorimetry in a Wide Context - Differential Scanning Calorimetry, Isothermal Titration Calorimetry and Microcalorimetry. InTech, 2013. http://dx.doi.org/10.5772/52109.
Повний текст джерелаТези доповідей конференцій з теми "HTPB propellants"
Brewster, M., G. Knott, and B. Chorpening. "Combustion of AP/HTPB laminate propellants." In 37th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-4501.
Повний текст джерелаde Flon, John, Sten Andreasson, Mattias Liljedahl, Carl Oscarson, Marita Wanhatalo, and Niklas Wingborg. "Solid Propellants based on ADN and HTPB." In 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-6136.
Повний текст джерелаHickman, S., and M. Brewster. "Oscillatory combustion of fine-AP/HTPB propellants." In 36th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-557.
Повний текст джерелаBAKER, P., A. MELLOR, and C. COFFEY. "Critical impact initiation energies for three HTPB propellants." In 26th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-2196.
Повний текст джерелаBoteler, J. M., and A. J. Lindfors. "Shock Loading Studies of AP/AL/HTPB Based Propellants." In 42ND ANNUAL REVIEW OF PROGRESS IN QUANTITATIVE NONDESTRUCTIVE EVALUATION: Incorporating the 6th European-American Workshop on Reliability of NDE. AIP Publishing LLC, 1996. http://dx.doi.org/10.1063/1.50832.
Повний текст джерелаMullen, J., and M. Brewster. "Investigation of Aluminum Agglomeration in AP/HTPB Composite Propellants." In 44th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-280.
Повний текст джерелаThomas, James C., Felix A. Rodriguez, Thomas Sammet, Catherine A. Dillier, Erica D. Petersen, and Eric L. Petersen. "Manufacturing and Burning of Composite AP/HTPB/AP Laminate Propellants." In AIAA Propulsion and Energy 2019 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-4365.
Повний текст джерелаThomas, James C., Felix A. Rodriguez, and Eric L. Petersen. "Strand Burner Experiments with Metal-Loaded AP/HTPB Laminate Propellants." In AIAA Scitech 2020 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2020. http://dx.doi.org/10.2514/6.2020-1429.
Повний текст джерелаJohn, Henry J., Frank E. Hudson, and Rodney Robbs. "High strain rate testing of AP/Al/HTPB solid propellants." In The tenth American Physical Society topical conference on shock compression of condensed matter. AIP, 1998. http://dx.doi.org/10.1063/1.55554.
Повний текст джерелаde Almeida, Luiz Eduardo N., Rene F. Goncalves, Jose A. Rocco, Fabio L. Calciolari, and Koshun Iha. "Evaluation of Plateau Burning Behavior in HTPB-AP-Al Composite Propellants." In AIAA Propulsion and Energy 2020 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2020. http://dx.doi.org/10.2514/6.2020-3901.
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