Study on the negative thrust of the underwater solid rocket engines

Engineering

• Boundary Condition 50%
• Burning Rate 50%
• Compressed Gas 50%
• Couplings 100%
• Inertia Effect 50%
• Initial Stage 50%
• Inlet Nozzle 50%
• Nozzle Exit 50%
• Numerical Methods 50%
• Pressure Difference 50%
• Solid Rocket Engine 100%