固体火箭发动机推进剂/衬层界面贮存性能研究进展

Engineering

• Crack Propagation 100%
• Rocket Engine 100%
• Performance Failure 100%
• Computer Simulation 50%
• Engineering 50%
• Test Method 50%
• Technical Approach 50%
• Inhibition 50%
• Scale Cross 50%
• Adaptability 50%
• Performance Parameter 50%
• Debonding 50%
• Characterization Method 50%
• Failure Analysis 50%
• Interface Crack 50%
• Stabilizer 50%
• Microlevel 50%
• Macro Level 50%

Material Science

• Crack Propagation 100%
• Stabilizer (Agent) 50%
• Debonding 50%
• Plasticizer 50%