The invention belongs to the field of lightweight
ablation-resistant dissipation heat-proof composite materials, particularly relates to an
ablation-resistant dissipation agent and application and aims to solve problems of high linear
ablation rate and
low dissipation agent content in a matrix of a dissipation heat-proof
composite material. A dissipation agent
alloy system comprises aluminum,
silicon and
boron, and the ternary dissipation agent is applied to the dissipation heat-proof
composite material. An application method includes: firstly, dissipation agent preparation; secondly, base material treatment; thirdly,
graphite crucible treatment; fourthly, vacuum
gas pressure infiltration. The novel ternary dissipation agent is provided on the basis of a dissipation heatproof mechanism, aliquid
ceramic protective layer for heat dissipation and
oxygen dissipation can be formed under conditions of high temperature,
high pressure and high-speed
particle flow erosion, and the prepared lightweight ablation-resistant dissipation heat-proof
composite material is used for manufacturing of
throat inserts of
solid rocket engine nozzles, gas rudders, end caps, wing leading edges and
tail vanes of hypersonic aircrafts and steering porous plate components of missiles.