Relevant bibliographies by topics / Hydroxyl Terminated Polybutadiene

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  1. Journal articles
  2. Dissertations / Theses
  3. Book chapters
  4. Conference papers

Academic literature on the topic 'Hydroxyl Terminated Polybutadiene'

Author: Grafiati
Published: 4 June 2021
Last updated: 6 September 2023

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Journal articles on the topic "Hydroxyl Terminated Polybutadiene"

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Vilar, W. D., S. M. C. Menezes, and P. R. Seidl. "Hydroxyl-terminated polybutadiene." Polymer Bulletin 38, no. 3 (1997): 327–32. http://dx.doi.org/10.1007/s002890050055.

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Vilar, W. D., S. M. C. Menezes, and L. Akcelrud. "Characterization of hydroxyl-terminated polybutadiene." Polymer Bulletin 33, no. 5 (1994): 557–61. http://dx.doi.org/10.1007/bf00296164.

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Vilar, W. D., S. M. C. Menezes, and L. Akcelrud. "Characterization of hydroxyl-terminated polybutadiene." Polymer Bulletin 33, no. 5 (1994): 563–70. http://dx.doi.org/10.1007/bf00296165.

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Vilar, W. D., S. M. C. Menezes, and L. Akcelrud. "Characterization of hydroxyl-terminated polybutadiene." Polymer Bulletin 35, no. 4 (1995): 481–88. http://dx.doi.org/10.1007/bf00297615.

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Vilar, W. D., S. M. C. Menezes, and P. R. Seidl. "Characterization of hydroxyl-terminated polybutadiene." Polymer Bulletin 38, no. 3 (1997): 311–18. http://dx.doi.org/10.1007/s002890050053.

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Vilar, W. D., M. T. M. Moutinho, S. M. C. Menezes, and F. M. B. Coutinho. "Characterization of hydroxyl-terminated polybutadiene." Polymer Bulletin 38, no. 3 (1997): 319–25. http://dx.doi.org/10.1007/s002890050054.

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Esker, D. R., and M. Q. Brewster. "Laser pyrolysis of hydroxyl-terminated polybutadiene." Journal of Propulsion and Power 12, no. 2 (1996): 296–301. http://dx.doi.org/10.2514/3.24027.

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Lee, Sangmook, In-Kwon Hong, Jae Wook Lee, and Won Bok Jeong. "Rheology and Curing of Hydroxyl Terminated Polybutadiene/(Sugar or Calcium Carbonate) Suspension." Polymer Korea 38, no. 4 (2014): 417–24. http://dx.doi.org/10.7317/pk.2014.38.4.417.

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Liu, Yahao, Jian Zheng, Xiao Zhang, et al. "Hyperbranched polyamide modified graphene oxide-reinforced polyurethane nanocomposites with enhanced mechanical properties." RSC Advances 11, no. 24 (2021): 14484–94. http://dx.doi.org/10.1039/d1ra00654a.

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We successfully modified graphene oxide with amino-terminated hyperbranched polyamide (HGO), and obtained a high-performance composite with enhanced strength and elongation at break via cross-linking hydroxyl-terminated polybutadiene chains with HGO.
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Mayen, Michel. "MIXING OF HYDROXYL-TERMINATED POLYBUTADIENE AND BORON." International Journal of Energetic Materials and Chemical Propulsion 2, no. 1-6 (1991): 190–95. http://dx.doi.org/10.1615/intjenergeticmaterialschemprop.v2.i1-6.80.

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Dissertations / Theses on the topic "Hydroxyl Terminated Polybutadiene"

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Peterson, Zachary W. "Closed-Loop Thrust and Pressure Profile Throttling of a Nitrous Oxide/Hydroxyl-Terminated Polybutadiene Hybrid Rocket Motor." DigitalCommons@USU, 2012. https://digitalcommons.usu.edu/etd/1400.

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Hybrid motors that employ non-toxic, non-explosive components with a liquid oxidizer and a solid hydrocarbon fuel grain have inherently safe operating characteristics. The inherent safety of hybrid rocket motors offers the potential to greatly reduce overall operating costs. Another key advantage of hybrid rocket motors is the potential for in-flight shutdown, restart, and throttle by controlling the pressure drop between the oxidizer tank and the injector. This research designed, developed, and ground tested a closed-loop throttle controller for a hybrid rocket motor using nitrous oxide and h
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Huang, Shih-Liang, and 黃世梁. "Hydroxyl terminated polybutadiene based polyurethane membranes." Thesis, 1996. http://ndltd.ncl.edu.tw/handle/24630465775396935934.

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博士<br>中原大學<br>化學工程研究所<br>84<br>In this study, hydoxyl terminated polybutadiene (HTPB) based Polyurethanes (PU) were synthesized. There are many morphological variations resulted from the aggregation of hard and soft segment in these nonpolar HTPB based membranes, which can be manipulated by varying composition, hard segment content, types of diisocyanate, or by introducing crosslinkage between soft segments, BPO content, metal salt complexation, IPN formation with 4-VP monomer and preparati
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Huang, Yu-Chin, and 黃育群. "The Preparation and Properties of Hydroxyl-Terminated Polybutadiene Graft Copolymer." Thesis, 2002. http://ndltd.ncl.edu.tw/handle/81013585759311037912.

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碩士<br>中原大學<br>化學研究所<br>90<br>There is no chemical bonding between the burn-rate modifier (ferrocene) and the binder (HTPB),if they are mixing together in product. In order to avoid the migration,it must form a effective chemical bonding.must In our study, the graft copolymer would be prepared by atom transfer radical polymerization (ATRP) and borane chemistry. Form the analysis of 1H-NMR, we can calculated the ratio of ferrocene grafted on HTPB. These graft copolymers have been characterized by IR, NMR, TGA and GPC. The applicability of HTPB is limited by its compatibility with other material.
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Chang, Po-Hsueh, and 張博學. "Properties and Pervaporation Performances of Hydroxyl terminated polybutadiene based polyurethane membranes." Thesis, 2007. http://ndltd.ncl.edu.tw/handle/98315212618499331031.

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碩士<br>國立勤益技術學院<br>化工與材料工程系<br>95<br>The main studies of this dissertation are divided into three parts : (1) properties and pervaporation performances of crosslinked HTPB-based polyurethane membranes. (2) properties and pervaporation separation of HTPB-based PU / PMMA IPNs (interpenetrating polymer networks) membranes. (3) properties of the HTPB-based PU blends with poly(vinyl chloride). First part of this thesis：PU solutions with different equivalent ratio of H12MDI / HTPB / 1,4-BD and NCO/OH equivalent ratio from 1.0 to 1.5 are synthesized by two-stages process. There are many morpholo
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Chen, Li-Heng, and 陳立恒. "Synthesis and Characterization of Hydroxyl Terminated Polybutadiene Grafted with Ferrocene Derivative." Thesis, 2012. http://ndltd.ncl.edu.tw/handle/02454432297983583170.

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碩士<br>國立臺灣大學<br>化學工程學研究所<br>100<br>Butacene, which can be prepared in a series of reactions, has been used in solid propellant composite as a catalyst to control the burning-rate of a rocket. At first, we synthesized 4-chlorobutylferrocene by using Friedel-Crafts acylation of ferrocene followed by deoxigenation of the acylated ferrocene. The resulting 4-chlorobutylferrocene was to react with magnesium metal by using Grignard reaction to form a corresponding Grignard intermediate compound which can react with chlorodimethylsilane to produce 4-(ferrocenylbutyl) dimethylsilane. Ferrocenehydrosila
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Yang, Chi-Rung, and 楊奇融. "Process Optimization and Mechanical Properties of Hydroxyl-terminated Polybutadiene Fuel Grain for Hybrid Propulsion." Thesis, 2015. http://ndltd.ncl.edu.tw/handle/49wspy.

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碩士<br>國立交通大學<br>機械工程系所<br>103<br>Hybrid rocket propulsion has been an important research subject for the past few years because of some outstanding characteristics such as system simplicity, high operation safety, and thrust controllability. In hybrid propulsion system, one of the commonest fuel grains is Hydroxyl-terminated Polybutadiene (HTPB). To design a stable hybrid propulsion system, complete characterization of the material properties of HTPB grain is necessary. In this thesis, baseline and advanced processes of preparing fuel grain are developed and tested. For the baseline process, w
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Chou, Tzu-Hao, and 周子豪. "Numerical and Experimental Investigation of Single-Port Hybrid Rocket Propulsion System with Nitrous Oxide and Hydroxyl-terminated Polybutadiene (HTPB) using Mixing Enhancer(s)." Thesis, 2015. http://ndltd.ncl.edu.tw/handle/28dagq.

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博士<br>國立交通大學<br>機械工程系所<br>103<br>Recently, hybrid rocket propulsion has attracted much attention because of many advantages, including high safety, high performance and low cost. Hybrid rocket system has better propulsion performance as compared to solid rocket system, but combustion efficiency of diffusion flame is generally low because of poor mixing between fuel and oxidizer. Thus, how to improve the mixing efficiency between fuel and oxidizer while keeping the simplicity of the system is one of the major research topics in hybrid propulsion. In this thesis, mixing enhancers are proposed to
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Sekkar, V. "Studies On HTPB Based Copolyurethanes As Solid Propellant Binders : Characterization And Modeling Of Network Parameters." Thesis, 1996. https://etd.iisc.ac.in/handle/2005/1569.

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Sekkar, 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.

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Book chapters on the topic "Hydroxyl Terminated Polybutadiene"

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Wohlfarth, Ch. "Solubility parameter of polybutadiene, hydroxyl terminated." In Polymer Solutions. Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-02890-8_882.

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Colclough, M. E., and N. C. Paul. "Nitrated Hydroxy-Terminated Polybutadiene: Synthesis and Properties." In ACS Symposium Series. American Chemical Society, 1996. http://dx.doi.org/10.1021/bk-1996-0623.ch010.

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"Flash Pyrolysis of Ammonium Perchlorate-Hydroxyl-Terminated-Polybutadiene Mixtures Including Selected Additives." In Solid Propellant Chemistry, Combustion, and Motor Interior Ballistics. American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/5.9781600866562.0003.0032.

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Almeida, 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. IGI Global, 2018. http://dx.doi.org/10.4018/978-1-5225-2903-3.ch010.

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The thermal decomposition kinetics of ammonium perchlorate (AP)/hydroxyl-terminated-polybutadiene (HTPB) samples, with Iron Oxide catalyst at nano and micro scale were studied by thermal analysis techniques at different heating rates in dynamic nitrogen atmosphere. The exothermic reaction kinetics was studied by differential scanning calorimetry (DSC) in isothermal conditions. The Arrhenius kinetic parameters were obtained by Flynn-Wall and Ozawa Kissinger and Starink methods. The propellant samples thermal decomposition was studied simultaneously by TG-DTA. For this purpose, solid propellant grains containing nano and micro scale iron oxide were formulated. The effect of catalysts on the propellant burning rate and the propellant initiation sensitivity were also evaluated by friction and impact. The effect of the catalyst in the propellant binder reaction was evaluated by viscosity and mechanical properties. SEM/EDS technique was used to evaluate the iron oxide morphology. Three bench firing tests were performed with rockets motor in order to know the ballistics parameters.
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Conference papers on the topic "Hydroxyl Terminated Polybutadiene"

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Krishnan, S., and K. Rajesh. "Erosive burning of ammonium perchlorate/hydroxyl-terminated-polybutadiene propellants under supersonic crossflows." In 37th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-3580.

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Rajesh, Kannalath Krishnan. "Thrust Modulation in a Nitrous Oxide/Hydroxyl-Terminated Polybutadiene Hybrid Rocket Motor." In 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-4503.

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Wright, Andrew, Calvin Cox, Abhijit Bhattacharyya, and M. Hudson. "Preliminary Characterization of Material Properties of Hydroxyl-Terminated Polybutadiene (HTPB) Solid Propellant." In 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-4460.

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Raissi, Sahson, and Joseph Kalman. "Investigation of Hydroxyl-terminated Polybutadiene Droplets Impacting Ammonium Perchlorate and Polytetrafluoroethylene Surfaces." In AIAA SCITECH 2022 Forum. American Institute of Aeronautics and Astronautics, 2022. http://dx.doi.org/10.2514/6.2022-2616.

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Gonçalves, Rene F., Koshun Iha, and Jose A. Rocco. "Enhancement of Ammonium Perchlorate/Hydroxyl-Terminated Polybutadiene Combustion Kinetics Using Ethanol-Doped Air." In 51st AIAA/SAE/ASEE Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-3869.

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Wibowo, Heri Budi, Widhi Cahya Dharmawan, Saeri, Ratih Sanggra Murti Wibowo, and Adi Yulianto. "Rapid analysis of HTPB (hydroxyl terminated polybutadiene) properties with infrared spectroscopy and gel chromatography." In PROCEEDINGS OF THE 3RD INTERNATIONAL SEMINAR ON METALLURGY AND MATERIALS (ISMM2019): Exploring New Innovation in Metallurgy and Materials. AIP Publishing, 2020. http://dx.doi.org/10.1063/5.0002819.

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Robles, Luis R., Johnny Ho, Bao Nguyen, et al. "Conceptual Regenerative Nozzle Cooling Design for a Hydroxyl-Terminated Polybutadiene and Oxygen Hybrid Rocket Engine." In ASME 2017 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/detc2017-68396.

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Regenerative rocket nozzle cooling technology is well developed for liquid fueled rocket engines, but the technology has yet to be widely applied to hybrid rockets. Liquid engines use fuel as coolant, and while the oxidizers typically used in hybrids are not as efficient at conducting heat, the increased renewability of a rocket using regenerative cycle should still make the technology attractive. Due to the high temperatures that permeate throughout a rocket nozzle, most nozzles are predisposed to ablation, supporting the need to implement a nozzle cooling system. This paper presents a proof-
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Donoughue, Mitchell, James Plotzke, and Monique McClain. "Adhesion of Thermoplastic Copolymers with Hydroxyl Terminated Polybutadiene in Application to Dissimilar Materials 3D Printing." In AIAA SCITECH 2023 Forum. American Institute of Aeronautics and Astronautics, 2023. http://dx.doi.org/10.2514/6.2023-2556.

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Donoughue, Mitchell, James Plotzke, and Monique McClain. "Correction: Adhesion of Thermoplastic Copolymers with Hydroxyl Terminated Polybutadiene in Application to Dissimilar Materials 3D Printing." In AIAA SCITECH 2023 Forum. American Institute of Aeronautics and Astronautics, 2023. http://dx.doi.org/10.2514/6.2023-2556.c1.

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Miller, Jacob K., and Jeffrey F. Rhoads. "Thermal and Mechanical Responses of Particulate Composite Plates Under Direct Excitation." In ASME 2013 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/detc2013-12138.

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The thermal and mechanical near-resonant responses of particulate composite plates formed from hydroxyl-terminated polybutadiene (HTPB) binder and varying volume ratios of NH4CL crystals (50, 65, 75%) are investigated. Each plate is mounted and forced with three levels of band-limited, white noise excitation (10–1000 Hz at 1.00, 1.86 and 2.44 g RMS). The mechanical response of each plate is recorded via scanning laser Doppler vibrometry. The plates are then excited at a single resonant frequency and the thermal response is recorded via infrared thermography. Comparisons are made between the me
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