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Ageing Behaviour of HTPB Based Rocket Propellant Formulations

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Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The ageing of HTPB propellant formulations containing nanoAl is investigated. During natural ageing the material undergoes a series of slow physico-chemical degradation reactions. By using accelerated ageing conditions it is possible to simulate the material behaviour at different time-temperature conditions especially focused on the in-service conditions. The mechanical and ageing behaviour of aluminised solid rocket propellants were investigated in terms of uniaxial tensile strength, DMA measurements, impact and friction sensitivity tests, SEM analyses.
Słowa kluczowe
Rocznik
Strony
149--165
Opis fizyczny
Bibliogr. 14 poz.
Twórcy
autor
autor
autor
autor
  • Fraunhoher Institut für Chemische Technologie (ICT) Postfach 1240, D-76318, Pfnztal-Berghausen, Germany
Bibliografia
  • [1] Layton L.H., Chemical structural aging studies on an HTPB propellant, AFRPLTR-75-13, 1975.
  • [2] Lillo F., D´Andrea B., Marcelli G., Sebasta A., Long Term Aging of Aerospace and Tactical SRM. Experimental Study, 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 8-11 July, Salt Lake City, Utah, 2001, AIAA Paper 2001-3284.
  • [3] Sbriccoli E., Salterelli R., Martinucci S., Comparison between Accelerated and Natural Aging, 20th International Annual Conference of ICT and 18th Annual Technical Meeting of GUS, 27-30 June, Karlsruhe, Germany, 1989.
  • [4] Kivity M., Hartman G., Achlama A.M., Aging of HTPB Propellant, 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 10-13 July, Tucson, Arizona, 2005, AIAA Paper 2005-3802.
  • [5] Bohn M.A., Prediction of Equivalent Time-Temperature Loads for Accelerated Ageing to Simulate Preset In-Storage Ageing and Time-Temperature Profile Loads, 40th International Annual Conference of ICT, 23-26 June, Karlsruhe, Germany, 2009, paper 78.
  • [6] Shalom A., Aped H., Kivity M., Horowitz D., The Effect of Nanosized Aluminum on Composite Propellant Properties, 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 10-13 July, Tucson, Arizona, 2005, AIAA Paper 2005-3604.
  • [7] Bui D.T., Atwood A. I., Atienzamoore T.M., Effect of Aluminum Particle Size on Combustion Behavior of Aluminized Propellants in PCP Binder, 35th International Annual Conference of ICT, 29 June-2 July, Karlsruhe, Germany, 2004, paper 27.
  • [8] Cliff M., Tepper F., Lisetsky V., Ageing Characteristics of Alex® Nanosize Aluminum, 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 8-11 July, Salt Lake City, Utah, 2001, AIAA Paper 2001-3287.
  • [9] Meda L., Marra G., Galfetti L., Severini F., DeLuca L.T., Nano-aluminum as energetic material for rocket propellants, Material Science and Engineering C, 2007, 27, 1393-1396.
  • [10] Brousseau P., Crête J.P., Dubois C., Ageing of Polymer-Coated Ultra-Fine Particles, 36th International Annual Conference of ICT and 32nd International Pyrothecnics Seminar, 28 June-1 July, Karslruhe, Germany, 2005, paper 89.
  • [11] de la Fuente J.L., Fernández-García M., Cerrada M.L., Viscoelastic Behavior In a Hydroxyl-Terminated Polybutadiene Gum and Its Highly Filled Composites: Effect on the Type of Filler on the Relaxation Processes, Journal of Applied Polymer Science, 2003, 88, 1705-1712.
  • [12] de la Fuente J.L., Rodrìguez O., Dynamic Mechanical Study on the Thermal Aging of a Hydroxyl-Terminated Polybutadiene-Based Energetic Composite, Journal of Applied Polymer Science, 2003, 87, 2397-2405.
  • [13] Ramier J., Gauthier C., Chazeau L., Stelandre L., Guy L., Payne Effect in Silica- Filled Styrene-Butadiene Rubber : Influence of Surface Treatment, Journal of Polymer Science : Part B : Polymer Physics, 2007, 45, 286-298.
  • [14] Tsagaropoulus G., Eisenberg A., Dynamic Mechanical Study of the Factors Affecting the Two Glass Transition Behavior of Filled Polymers. Similarities and Differences with Random Ionomers, Macromolecules, 1995, 28, 6067-6077.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BAT1-0034-0029
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