Multidisciplinary optimization of a solid propellant sectional geometry for internal ballistic and structural strength criteria

Keyphrases

• ABAQUS Software 50%
• Ballistic 50%
• Chamber Pressure 50%
• Design Alternatives 50%
• Deterministic Approach 50%
• Finite Element Method 50%
• Geometric Design 50%
• Geometrical Parameters 50%
• Internal Ballistic Performance 50%
• Internal Ballistics 100%
• Linear Viscoelastic Model 50%
• Multidisciplinary Design Optimization 100%
• Optimization Study 50%
• Parameter Values 50%
• Process Optimization 50%
• Propellant 100%
• Solid Propellant 100%
• Solid Propellant Grain 50%
• Solid Rocket Motor 50%
• Structural Strength 50%
• Structural Strength Criterion 100%

Engineering

• Abaqus 50%
• Chamber Pressure 50%
• Design Alternative 50%
• Finite Element Analysis 50%
• Geometrical Parameter 50%
• Internals 100%
• Linear Viscoelastic Model 50%
• Rocket Engine 50%
• Strength Criterion 100%
• Structural Strength 100%