Effect of Wollastonite on the ablation resistance of EPDM based elastomeric heat shielding materials for solid rocket motors

[1]  J. Kenny,et al.  Effect of boron carbide nanoparticles on the thermal stability of carbon/phenolic composites , 2017 .

[2]  Heath T. Martin.  Assessment of the performance of ablative insulators under realistic solid rocket motor operating conditions , 2017 .

[3]  J. Kenny,et al.  Ablation modeling of state of the art EPDM based elastomeric heat shielding materials for solid rocket motors , 2016 .

[4]  M. Abdollahi,et al.  Effect of borax on the thermal and mechanical properties of ethylene-propylene-diene terpolymer rubber-based heat insulator , 2015 .

[5]  M. Natali,et al.  Compressive char strength of thermoplastic polyurethane elastomer nanocomposites , 2014 .

[6]  O. Ezekoye,et al.  An in-situ ablation recession sensor for carbon/carbon ablatives based on commercial ultra-miniature thermocouples , 2014 .

[7]  Huawei Zou,et al.  Thermal stability and ablation properties study of aluminum silicate ceramic fiber and acicular wollastonite filled silicone rubber composite , 2014 .

[8]  J. Kenny,et al.  EPDM based heat shielding materials for Solid Rocket Motors: A comparative study of different fibrous reinforcements , 2013 .

[9]  Dezhen Wu,et al.  Surface-Modified Polyimide Fiber-Filled Ethylenepropylenediene Monomer Insulations for a Solid Rocket Motor: Processing, Morphology, and Properties , 2013 .

[10]  S. Hoa,et al.  Thermal insulation by heat resistant polymers for solid rocket motor insulation , 2012 .

[11]  J. Kenny,et al.  Ablative properties of carbon black and MWNT/phenolic composites: A comparative study , 2012 .

[12]  Eric Allcorn,et al.  Ablation performance and characterization of thermoplastic polyurethane elastomer nanocomposites , 2011 .

[13]  V. I. Shumskii,et al.  Particulars of thermally stimulated gas-release from silica glass fiber , 2011 .

[14]  B. Lattimer,et al.  Thermal Response of Composite Materials to Elevated Temperatures , 2011 .

[15]  J. Kenny,et al.  A nanostructured ablative bulk molding compound: Development and characterization , 2011 .

[16]  H. Doyle.  Development of Design Data for the Application of Phenolic Asbestos Laminates on Fire Vehicle Heat Protective Systems , 2011 .

[17]  J. Kenny,et al.  Synthesis and thermal characterization of phenolic resin/silica nanocomposites prepared with high shear rate‐mixing technique , 2011 .

[18]  K. Mehrdad,et al.  NUMERICAL AND EXPERIMENTAL EVALUATIONS OF THE FLAMMABILITY AND PYROLYSIS OF A RESOLE-BASED NANOCOMPOSITE BY CONE CALORIMETER , 2011 .

[19]  Hongti Zhang.  Comparison and Analysis of Thermal Degradation Process of Aramid Fibers (Kevlar 49 and Nomex) , 2010 .

[20]  Zhicheng Zhang,et al.  An excellent ablative composite based on PBO reinforced EPDM , 2010 .

[21]  J. Kenny,et al.  Phenolic matrix nanocomposites based on commercial grade resols: Synthesis and characterization , 2010 .

[22]  L. Pilato,et al.  Phenolic Resins: A Century of Progress , 2010 .

[23]  Zhicheng Zhang,et al.  Effect of fiber orientation angle on thermal degradation and ablative properties of short‐fiber reinforced EPDM/NBR rubber composites , 2009 .

[24]  A. Bahramian,et al.  Ablation mechanism of polymer layered silicate nanocomposite heat shield. , 2009, Journal of hazardous materials.

[25]  G. Sui,et al.  Ablation and thermal properties of ethylene–propylene–diene elastomer composites reinforced with polysulfonamide short fibers , 2009 .

[26]  G. Sui,et al.  Effects of pretreated polysulfonamide pulp on the ablation behavior of EPDM composites , 2008 .

[27]  A. Bahramian,et al.  Thermal Degradation Process of Resol Type Phenolic Matrix/Kaolinite Layered Silicate Nanocomposite , 2007 .

[28]  Manoj Gupta,et al.  Ethylene-propylene Diene Rubber as a Futuristic Elastomer for Insulation of Solid Rocket Motors , 2006 .

[29]  A. Bahramian,et al.  Ablation and thermal degradation behaviour of a composite based on resol type phenolic resin: Process modeling and experimental , 2006 .

[30]  B. Nagabhushana,et al.  Solution combustion derived nanocrystalline macroporous wollastonite ceramics , 2006 .

[31]  A. Bhowmick,et al.  Studies on thermal degradation of short melamine fibre reinforced EPDM, maleated EPDM and nitrile rubber composites , 2003 .

[32]  S. Bourbigot,et al.  Heat resistance and flammability of high performance fibres: A review , 2002 .

[33]  J. Hearle,et al.  High-performance Fibres , 2001 .

[34]  J. Kenny,et al.  Degradation behaviour of a composite material for thermal protection systems Part III Char characterization , 2000 .

[35]  C. Martin,et al.  Non-Asbestos Insulation Testing Using a Plasma Torch , 2000 .

[36]  Larry D. Allred,et al.  Asbestos Free Insulation Development for the Space Shuttle Solid Propellant Rocket Motor (RSRM) , 2000 .

[37]  Jose Maria Kenny,et al.  Degradation behaviour of a composite material for thermal protection systemsPart II Process simulation , 1998 .

[38]  J. Kenny,et al.  Degradation behaviour of a composite material for thermal protection systems Part I–Experimental characterization , 1998 .

[39]  A. Donskoy.  Elastomeric Heat-Shielding Materials for Internal Surfaces of Missile Engines , 1996 .

[40]  M. Bell,et al.  ASRM case insulation design and development , 1992 .

[41]  J. Koo,et al.  Performance of high-temperature composite ablatives under a hostile environment , 1992 .

[42]  Joseph H. Koo,et al.  Comparison of ablative materials in a simulated solid rocket exhaustenvironment , 1991 .

[43]  A. Bhowmick,et al.  Studies on the ageing of EPDM based rocket insulator compound by stress relaxation and the effect of propellant binder , 1988 .

[44]  A. Bhowmick,et al.  Thermal and ablative properties of rocket insulator compound based on EPDM , 1988 .

[45]  A. Bhowmick,et al.  Aging of EPDM rubber , 1987 .

[46]  A. Bhowmick,et al.  Ageing of rocket insulator compound based on EPDM , 1986 .

[47]  G. R. Moore,et al.  Determination of Kinetic Parameters for Thermal Decomposition of Phenolic Ablative Materials by Multiple Heating Rate Method , 1981 .

[48]  L. M. Hedges.  Development of improved asbestos reinforced phenolic insulating composites (optimization of physical properties as a function of molding technique and post cure conditions) , 1973 .

[49]  J. W. Youren.  Ablation of elastomeric composites for rocket motor insulation , 1971 .

[50]  R. C. Laramee,et al.  Development of low cost ablative nozzles for solid propellant rocket motors, volume 2 Final report , 1970 .

[51]  J. Winter,et al.  Rocket Engine Evaluation of Erosion and Char as Functions of Fabric Orientation for Silica-Reinforced Nozzle Materials. , 1969 .

[52]  Dominick V. Rosato,et al.  Environmental effects on polymeric materials , 1968 .

[53]  P. Gaines.  Improved method facilitates debulking and curing of phenolic impregnated asbestos , 1966 .

[54]  H. Seifert,et al.  Rocket Propulsion Elements , 1963 .

[55]  D. S. Carton,et al.  Rocket propulsion technology , 1961 .

[56]  F. Pundsack.  The Properties of Asbestos. I. The Colloidal and Surface Chemistry of Chrysotile. , 1955 .