49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2013
DOI: 10.2514/6.2013-3864
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An Investigation of Compressive and Shear Strength of Char from Polymer Nanocomposites for Propulsion Applications

Abstract: Ablative material is used in solid rocket motors (SRMs), since the formation of a char layer provides thermal protection to key structural components during motor firings. The char strength of thermoplastic polyurethane elastomer nanocomposites (TPUNs) is of particular interest due to its potential as a replacement for the current industry standard, Kevlar®-filled EPDM. TPUNs are being considered to replace Kevlar®-filled EPDM for a number of reasons, primarily because: TPUNs exhibit superior ablation and insu… Show more

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“…The clamping mechanism should not only adapt to the sample shape but also create little or no bending stress on the sample as the material is very fragile. The clamping mechanism concept has been implemented on the shear strength version of the developed tester . New protocols to elaborate data could be considered: as an example, because the material that has thicker char layers will inherently require more energy to crush the char, then in order to compare the char strength of different specimens more accurately, the energy can be normalized by the thickness of the char.…”
Section: Discussionmentioning
confidence: 99%
“…The clamping mechanism should not only adapt to the sample shape but also create little or no bending stress on the sample as the material is very fragile. The clamping mechanism concept has been implemented on the shear strength version of the developed tester . New protocols to elaborate data could be considered: as an example, because the material that has thicker char layers will inherently require more energy to crush the char, then in order to compare the char strength of different specimens more accurately, the energy can be normalized by the thickness of the char.…”
Section: Discussionmentioning
confidence: 99%