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Optimization of network forming agents for different types of composite propellant grain

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
There has been a constant endeavour to improve the mechanical properties of hydroxyterminated polybutadiene (HTPB)-based, composite solid propellants. In order to have a better understanding of the requirements, a systematic study has been conducted on the effects of varying the network forming agents on the mechanical properties of nitramine based composite propellants. Under this scheme, a series of compositions was formulated using various chain extenders [1,6-hexanediol (HD) and 1,4-butanediol (BD)] and cross linkers [1,2,6-hexanetriol (HT) and trimethylolpropane (TMP)] in different proportions. Propellant formulation experiments were conducted wherein the network forming agent composition was systematically varied to achieve the maximum possible strain capability and moderately high tensile strength, keeping the weight % of the network forming agents and other ingredients constant. The mechanical properties (% elongation, tensile strength and elastic-modulus) of the finished propellant have been plotted vs. formulation number; this can be used to select a suitable network forming agent composition for a specified grain architecture and application. Network forming agents containing 1,2,6-hexanetriol provide a high elastic-modulus (120 kg/cm2) and a high tensile strength (~12 kg/cm2), which can be used in free standing grains. Network forming agents based on 1,6-hexanediol and 1,2,6-hexanetriol (in 1:1 proportion by weight) give high elongation (~50%) and a moderately high tensile strength (~9 kg/cm2), useful for case bonded propellant grains.
Rocznik
Strony
409--417
Opis fizyczny
Bibliogr. 16 poz., rys., tab.
Twórcy
autor
  • High Energy Material Research Laboratory, Sutarwadi, Pune-411021, India
autor
  • High Energy Material Research Laboratory, Sutarwadi, Pune-411021, India
autor
  • High Energy Material Research Laboratory, Sutarwadi, Pune-411021, India
autor
  • High Energy Material Research Laboratory, Sutarwadi, Pune-411021, India
Bibliografia
  • [1] Krishnan S., Chakravarthy S.R., Athithan S.K., Propellant and Explosives Technology, Allied Publishers, 1998, pp. 152.
  • [2] Gomez A., Erisken C., Yilmazar U., Pekel F., Ozkar S., Mechanical and Burning Properties of Highly Loaded Composite Propellants, J. Appl. Polym. Sci, 1998, 67, 1457.
  • [3] Minoura Y., Yamashita S., Okamoto H., Matsuo T., Izawa M., Kohmoto S.I., Crosslinking and Mechanical Property of Liquid Rubber. 1. Curative Effect of Aliphatic Diols, J. Appl. Polym. Sci, 1978, 22, 1817.
  • [4] Ahn T.O., Uk Jung S, Mo Jeong H., Lee S.W., The Properties of Polyurethanes with Mixed Chain Extenders and Mixed Soft Segments, J. Appl. Polym. Sci, 1994, 51, 43.
  • [5] Minoura Y., Yamashita S., Okamoto H., Matsuo T., Izawa M., Kohmoto S.I., Crosslinking and Mechanical Properties of Liquid Rubber. III. Curative Effect of Aralkyl and Alicyclic Diol, J. Appl. Polym. Sci, 1978, 22, 3101.
  • [6] Minoura Y., Yamashita S., Okamoto H., Matsuo T., Izawa M., Kohmoto S.I., Crosslinking and Mechanical Property of Liquid Rubber. II. Curative Effect of Aromatic Diols, J. Appl. Polym. Sci, 1979, 23, 1137.
  • [7] Wang G., Ning J., Guo H., Shi Y., Wang Z., Technical Way of Improving the Mechanical Properties of Composite Propellant, Theory and Practice of Energetic Materials, Proc., 8th Int. Autumn Semin. on Propellants, Explosives and Pyrotechnics, Kunming, China, Sep.22-25, 2009, 8, 647-651.
  • [8] Radwan M.A., Stress Strain Properties of Nitramine Composite Rocket Propellants, 32nd Int. Annu. Conf. of ICT, Karlsruhe, 2001, 45/1-45/12.
  • [9] Haska S.B., Bayramli E., Pekel F., Ozkar S., Mechanical Properties of HTPB-IPDI-based Elastomers, J. Appl. Polym. Sci, 1997, 64(12), 2347-2354.
  • [10] Hocaoglu O., Ozbelge T., Pekel F., Ozkar S., Fine-tuning the Mechanical Properties of Hydroxy-terminated Polybutadiene/Ammonium Perchlorate-based Composite Solid Propellant by Varying the NCO/OH and Triol/Diol Ratios, J. Appl. Polym. Sci, 2002, 84, 2072.
  • [11] Manjari R., Somasundaran U.I., Joseph V.C., Sriram T., Structure-property Relationship of HTPB-based Propellants. II. Formulation Tailoring for Better Mechanical Properties, J. Appl. Polym. Sci, 1993, 48, 279.
  • [12] Manjari R., Joseph V.C., Pandureng L.P., Sriram T., Structure-property Relationship of TPB-based Propellants. I. Effect of Hydroxy Value of HTPB Resin, J. Appl. Polym. Sci, 1993, 48, 271.
  • [13] Stockler Pinto DVB., Rezende L.C., Kawamoto A.M., Julio de B., Domingues L. de A.K., Italo N., da Cruz S.M., Leal S.D., Formulation Tailoring of AP/HTPB Composite Propellants Containing a Polyamine-type Bonding Agent, 39th Int. Annu. Conf. of ICT, Karlsruhe, 2008, 79/1-79/12.
  • [14] Singh M., Kanungo B.K., Bansal T.K., Effect of Low Molecular Weight Diol and Triol on Hydroxy-terminated Polybutadiene Prepolymer Based Polyurethane Network Properties, Indian J. Eng. Mat. Sci, 2000, 7(5-6), 378-384.
  • [15] Patil M.S., Singh H., Ballistic and Mechanical Properties of HTPB Based Propellant, J. Hazard. Mater., 1998, 19, 271.
  • [16] Iqbal M.M., Liang W., Modelling the Moisture Effects of Solid Ingredients on Composite Propellant Properties, Aerospace Sci. Technol., 2006, 10, 695.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-03f53c3c-3b73-404a-ab52-81af7c21d567
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