General energetic burning rate catalyst, preparation method and application thereof
By synthesizing a general-purpose energetic combustion rate catalyst, the problem of the limited selectivity of existing catalysts has been solved, achieving efficient catalysis of various solid propellant components with high thermal stability and safety.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- XIAN MODERN CHEM RES INST
- Filing Date
- 2023-04-19
- Publication Date
- 2026-07-03
AI Technical Summary
Existing EMOFs-based energetic burning rate catalysts in solid propellants have the problem of relatively limited catalytic selectivity, failing to achieve excellent catalytic effects on a variety of propellant components.
A general-purpose energetic combustion rate catalyst was synthesized by reacting sodium azotetrazole with palladium acetate under specific conditions. The catalyst has a large specific surface area, high thermal stability and multidimensional structure, and is solvent-free, making it suitable for catalyzing various solid propellant components.
It significantly advances the thermal decomposition temperature of various existing energetic materials such as AP, RDX, HMX, CL-20 and DAP-4, with excellent catalytic effect, thermal decomposition peak temperature greater than 400℃, and high thermal stability and safety.
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Figure CN116574068B_ABST