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Studies of the Influence of Nano Iron(III) Oxide on Selected Properties of Solid Heterogeneous Propellants Based on HTPB

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
This paper presents the results of investigations into the use of 56 nm nano iron(III) oxide as a combustion rate modifier in a solid heterogeneous rocket propellant (SHRP). A series of solid heterogeneous rocket propellants based on HTPB and ammonium perchlorate with different nano iron(III) oxide contents in the propellant composition were prepared and investigated. The ballistic parameters of the examined propellants were determined by combustion in a laboratory rocket motor (LRM). The ballistic properties were evaluated in the pressure range 5-10 MPa. It was found that the linear burning rate at 7 MPa was increased by 15% for 1% nano iron(III) oxide content in comparison to 0.2% content. Determination of the sensitivity to friction and impact, the calorific value, hardness and decomposition temperature of the derived propellants were also investigated.
Rocznik
Strony
1051--1063
Opis fizyczny
Bibliogr. 19 poz., rys., tab.
Twórcy
autor
  • Institute of Industrial Organic Chemistry, Annopol 6, 03-236 Warsaw, Poland
  • Military University of Technology, Kaliskiego 2, 00-908 Warsaw, Poland
autor
  • Institute of Industrial Organic Chemistry, Annopol 6, 03-236 Warsaw, Poland
autor
  • Military University of Technology, Kaliskiego 2, 00-908 Warsaw, Poland
  • Institute of Industrial Organic Chemistry, Annopol 6, 03-236 Warsaw, Poland
Bibliografia
  • [1] Sutton G.P., Biblarz O., Rocket Propulsion Elements, Wiley-Interscience, New York, 2001, pp. 475-476; ISBN 0-471-32642-9.
  • [2] Bhowmik D., Sadavarte V.S., Pande S.M., Saraswat B.S., An Energetic Binder for the Formulation of Advanced Solid Rocket Propellants, Cent. Eur. J. Energ. Mater., 2015, 12(1), 145-158.
  • [3] Dey A., Ghorpade V.G., Kumar A., Gupta M., Biuret: a Potential Burning Rate Suppressant in Ammonium Chlorate(VII) Based Composite Propellants, Cent. Eur. J. Energ. Mater., 2014, 11(1), 3-14.
  • [4] Ghosh K., Behera S., Kumar A., Padale B.G., Deshpande D.G., Kumar A., Gupta M., Studies on Aluminized, High Burning Rate, Butacene® Based, Composite Propellants, Cent. Eur. J. Energ. Mater., 2014, 11(3), 323-333.
  • [5] Sangtyani R., Kumar A., Kumar A., Gupta M., Optimization of Network Forming Agents for Different Types of Composite Propellant Grain, Cent. Eur. J. Energ. Mater., 2013, 10(3), 409-438.
  • [6] Kubota N., Propellants and Explosives, Thermochemical Aspects of Combustion, Wiley-VCH, Weinheim, 2007; ISBN 3-527-30210-7.
  • [7] Gore G.M., Tipare K.R., Bhatewara R.G., Prasad U.S., Gupta M., Mane S.R., Evaluation of Ferrocene Derivatives as Burn Rate Modifiers in AP/HTPB-based Composite Propellants, Def. Sci. J., 1999, 49(2), 151-185.
  • [8] Pekel F., Pinardağ E., Türkan A., An Investigation of the Catalytic Effect of Iron(III) Oxide on the Burning Rate of Aluminized HTPB/AP Composite Propellant, 26th Int. Annu. Conf. ICT, Karslrue, 1995, 61.1-10.
  • [9] Styborski J.A., Scorza M.J., Smith M.N., Oehlschlaege M.A., Iron Nanoparticles Additives as Burning Rate Enhancers in AP/HTPB Composite Propellants, Propellants Explos. Pyrotech., 2015, 40, 253-299.
  • [10] Florczak B., Cudziło S., Catalytic Effect of Nano Fe2O3 on Burning Rate of Aluminized PBAN/AP/HMX Composite Propellant (in Polish), Biuletyn WAT, 2009, 58, 4.
  • [11] Patil P.R., Krishnamurthy V.N., Joshi S., Differential Scanning Calorimetric Study of HTPB Based Composite Propellants in Presence of Nano Ferric Oxide, Propellants Explos. Pyrotech., 2006, 31(6), 442.
  • [12] Lu K.-T., Yang T.-M., Li J.-S., Yeh T.-F., Study on the Burning Characteristics of AP/Al/HTPB Composite Solid Propellant Containing Nano-sized Ferric Oxide Powder, Combust. Sci. Technol., 2012, 184(12), 2100-2116.
  • [13] Florczak B., Sałaciński T., Maranda A., Sitkiewicz-Wołodko R., Test of Sensitivity of Two-bases Solid Homogeneous Propellants (in Polish), Przem. Chem., 2013, 92(8), 1464.
  • [14] Suceska M., Test Methods for Explosives, Springer-Verlag, New York, 1995; ISBN 978-1-4612-0797-9.
  • [15] Mining Explosives. Determination of the Decomposition Temperature (in Polish), The Specialized Norm BN-76/6091-08, 1976.
  • [16] Florczak B., Bogusz R., Skupiński W., Chmielarek M., Study of the Effect of Nitrated Hydroxy-terminated Polybutadiene (NHTPB) Content on the Properties of Heterogeneous Rocket Propellant, Cent. Eur. J. Energ. Mater., 2015, 12(4), 841-854.
  • [17] Florczak B., Białek M., Cholewiak A., Determination of the Internal Ballistic Properties of Solid Heterogeneous Rocket Propellants, Cent. Eur. J. Energ. Mater., 2014, 11(4), 589-601.
  • [18] Bogusz R., Magnuszewska P., Florczak B., Maranda A., Study of the Effect of Curing Agents on Properties of the Heterogeneous Solid Rocket Propellants (in Polish), Przem. Chem., 2015, 94(3), 366-368.
  • [19] Florczak B., Viscosity Testing of HTPB Rubber Based Pre-binders, Cent. Eur. J. Energ. Mater., 2014, 11(4), 625-637.
Uwagi
Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę (zadania 2017).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-67aa4c91-0e14-4c24-8455-4d1e292aa12a
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