Experimental Determination of Some Design Properties of Viscoelastic Solid Propellant Using Uniaxial Tensile Test
Adel, W., Kamal, H., El-Soualey, D. (2011). Experimental Determination of Some Design Properties of Viscoelastic Solid Propellant Using Uniaxial Tensile Test. EKB Journal Management System, 14(AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 14 – May 24 - 26, 2011), 1-11. doi: 10.21608/asat.2011.23407
W. M. Adel; H. Kamal; D. El-Soualey. "Experimental Determination of Some Design Properties of Viscoelastic Solid Propellant Using Uniaxial Tensile Test". EKB Journal Management System, 14, AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 14 – May 24 - 26, 2011, 2011, 1-11. doi: 10.21608/asat.2011.23407
Adel, W., Kamal, H., El-Soualey, D. (2011). 'Experimental Determination of Some Design Properties of Viscoelastic Solid Propellant Using Uniaxial Tensile Test', EKB Journal Management System, 14(AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 14 – May 24 - 26, 2011), pp. 1-11. doi: 10.21608/asat.2011.23407
Adel, W., Kamal, H., El-Soualey, D. Experimental Determination of Some Design Properties of Viscoelastic Solid Propellant Using Uniaxial Tensile Test. EKB Journal Management System, 2011; 14(AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 14 – May 24 - 26, 2011): 1-11. doi: 10.21608/asat.2011.23407

Experimental Determination of Some Design Properties of Viscoelastic Solid Propellant Using Uniaxial Tensile Test

International Conference on Aerospace Sciences and Aviation Technology
Article 93, Volume 14, AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 14 – May 24 - 26, 2011, May 2011, Page 1-11  XML PDF (524.67 K)
Document Type: Original Article
DOI: 10.21608/asat.2011.23407
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Authors
W. M. Adel1; H. Kamal1; D. El-Soualey2
1Egyptian Armed Forces, Egypt.
2Professor, High Institute of Technology of 10th Ramadan, October Branch, Egypt.
Abstract
An experimental data treatment is introduced to manage with the tensile test responses of highly non-linear viscoelastic materials. This work investigates the effects of strain rate and temperature on the behaviour of solid propellant treated as non-linear viscoelastic material. The material investigated was rubber composite based on hydroxylterminated poly butadiene (HTPB).Viscoelastic design properties were derived from the experimentally measured tensile data. Design properties include isochronous stress–strain diagrams at different strain rates and temperatures.
Keywords
Solid propellant; Mechanical behavior; Non-linear viscoelastic; Strain rate
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