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Microcellular Oblate Propellant with Skin-core Structure Deterred by Poly(neopentanediol adipate)

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
In order to solve the issues of high muzzle flash, smoke, residue, migration rate and carcinogenicity of double-base oblate propellants deterred by dibutyl phthalate (DBP), skin-core structure microporous oblate propellants to replace DBP deterring technology were fabricated in the present work by supercritical carbon dioxide (SC-CO2) foaming technology. Poly(neopentanediol adipate) (NA) was employed as the deterrent to modify the combustion properties because of ist lower migration rate in storage. Scanning electron microscopy (SEM) was used to observe the morphology of the microporous oblate propellants generated by different processing conditions, and the combustion properties were investigated by closed bomb tests. The SEM images indicated that the skin region displayed smaller cell diameters and lower cell density compared with cells in the core region. The closed bomb tests demonstrated that it was feasible to adjust the progressive combustion performance by controlling the skin-core structure and the NA deterred layer. The burning time values of the original, the microcellular, and the NA deterred samples were 3.45, 2.14, and 4.20 ms, respectively. Microcellular oblate propellants, with a skin-core structure foamed by SC-CO2 and deterred by NA, provides a novel and promising method to realize progressive combustion performance.
Rocznik
Strony
49--65
Opis fizyczny
Bibliogr. 14 poz., rys., tab.
Twórcy
autor
  • Key Laboratory of Special Energy Materials (Nanjing University of Science and Technology), Ministry of Education, Nanjing 210094, China
  • School of Chemical Engineering, Nanjing University of Science and Technology, Nanjing 210094, China
autor
  • Key Laboratory of Special Energy Materials (Nanjing University of Science and Technology), Ministry of Education, Nanjing 210094, China
  • School of Chemical Engineering, Nanjing University of Science and Technology, Nanjing 210094, China
  • Key Laboratory of Special Energy Materials (Nanjing University of Science and Technology), Ministry of Education, Nanjing 210094, China
  • School of Chemical Engineering, Nanjing University of Science and Technology, Nanjing 210094, China
autor
  • Key Laboratory of Special Energy Materials (Nanjing University of Science and Technology), Ministry of Education, Nanjing 210094, China
  • School of Chemical Engineering, Nanjing University of Science and Technology, Nanjing 210094, China
autor
  • Luzhou North Chemical Industry Co., Ltd., Luzhou 646003, China
autor
  • Luzhou North Chemical Industry Co., Ltd., Luzhou 646003, China
Bibliografia
  • [1] Wilson, K.; Wilson, M.; Poole, D.; Holland, G. Low Temperature Autoigniting Propellant Composition. Patent US 5866842, 1999.
  • [2] Verneker, V.; Kishore, K.; Subhas, C. Mechanism of Thermal Decomposition of Double Base Propellants. Propellants Explos. Pyrotech. 1983, 8(3): 77-79.
  • [3] Böhnlein-Mauß, J.; Kröber, H. The REACH Impact on Gun Propellant Formulations. Propellants Explos. Pyrot. 2017, 42(1): 54-61.
  • [4] Lelu, A.; Grignon, J.; Gonthier, B.; Tauzia, J. Combustion Inhibitor Based on an Aliphatic Polyurethane Elastomer for a Propellant, and Block Coated with this Inhibitor. Patent US 4638735, 1987.
  • [5] Shaowu, L.; Bo, L.; Shuang, Z.; Qionglin, W.; Qing, P.; Yuanbo, Z.; Bing, H.; Lun, W. Migration of Polymer Deterrent in Two Kinds of Propellants. Chin. J. Energ. Mater. 2010, 18(6): 635-638.
  • [6] Binbin, W.; Xin, L.; Zeshan, W.; DeLuca, L.T.; Zhitao, L.; Weidong, H. Effects of Particle Size and Morphology of NQ on Thermal and Combustion Properties of Triple-base Propellants. Combust. Flame 2018, 193: 123-132.
  • [7] Böhnlein-Mauß, J.; Eberhardt, A.; Fischer, T. Foamed Propellants. Propellants Explos. Pyrotech. 2002, 27(3): 156-160.
  • [8] Böhnlein-Mauß, J.; Kröber, H. Technology of Foamed Propellants. Propellants Explos. Pyrotech. 2009, 34(3): 239-244.
  • [9] Ping, W.; Lei, Z.; Xiangyang, L.; Wenfang, Z. Preparation of Nitrocellulose-based Micro-pores Spherical Powder by Solvent Leaching Method. Chin. J. Explos. Pyrot. 2005, 23(11): 1107-1110.
  • [10] Yang, W.; Li, Y.; Ying, S. An Investigation of the Preparation and Performance of Microcellular Combustible Material. Cent. Eur. J. Energ. Mater. 2014, 11(2):257-269.
  • [11] Yuxiang, L.; Yang, W.; Ying, S.; Jinhua, P. Combustion of Gas-permeable Gun Propellants. J. Energ. Mater. 2015, 33(3): 167-179.
  • [12] Wenlong, W.; Yajun, D.; Sanjiu, Y. Solubility of Supercritical Carbon Dioxide in Oblate Spherical Propellants. Acta Armamentarii 2018, 39(10): 1965-1970.
  • [13] Yajun, D.; Sanjiu, Y. Cell Structure, Density and Impact Strength of Cellulose Acetate Foamed with Supercritical Carbon Dioxide. Cell. Polym. 2015, 34(6): 339-352.
  • [14] Tsivintzelis, I.; Sanxaridou, G.; Pavlidou, E.; Panayiotou, C. Foaming of Polymers with Supercritical Fluids: a Thermodynamic Investigation. J. Supercrit. Fluid 2016, 110: 240-250.
Uwagi
Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2020).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-04155923-5335-4ac8-8256-12a4eb7ab0a6
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