A kind of deformable solid propellant and its preparation method
A solid propellant and curing agent technology, applied in the direction of offensive equipment, compressed gas generation, non-explosive/non-thermal agent components, etc., can solve the problems of poor adaptability and achieve the effect of changing performance
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Embodiment 1
[0025] A deformable solid propellant prepared from the following raw materials: oxidizing agent, reducing agent, shape memory binder, plasticizer and others.
[0026] The oxidant is ammonium perchlorate and ammonium dinitramide; the reducing agent is nano-aluminum powder and magnesium powder; the plasticizer is acetyl triethyl citrate; the shape memory adhesive is an epoxy matrix, a curing agent, and a catalyst And energy-containing additives; wherein the epoxy matrix is bisphenol A epoxy resin, the curing agent is thiocyanuric acid, the catalyst is 2-methylimidazole, the energy-containing additive is polyazide glycidyl ether (GAP), and others are : Alcohol amine complex, aluminate coupling agent, N,N-diphenyl-p-phenylenediamine, carbon black, catocine.
[0027] The mass ratio relationship of the above raw materials is: 50 parts of ammonium perchlorate, 2 parts of ammonium dinitramide, 10 parts of nano-aluminum powder, 1 part of magnesium powder; 3 parts of acetyl triethyl c...
Embodiment 2
[0029] A deformable solid propellant prepared from the following raw materials: oxidizing agent, reducing agent, shape memory binder, plasticizer and others.
[0030] The oxidant is ammonium perchlorate and ammonium dinitramide; the reducing agent is nano-aluminum powder and magnesium powder; the plasticizer is acetyl triethyl citrate; the shape memory adhesive is an epoxy matrix, a curing agent, and a catalyst And energy-containing additives; wherein the epoxy matrix is bisphenol A epoxy resin, the curing agent is thiocyanuric acid, the catalyst is 2-methylimidazole, the energy-containing additive is polyazide glycidyl ether (GAP), and others are : Alcohol amine complex, aluminate coupling agent, N,N-diphenyl-p-phenylenediamine, carbon black, catocine.
[0031] The mass ratio relationship of the above raw materials is: 60 parts of ammonium perchlorate, 4 parts of ammonium dinitramide, 15 parts of nano-aluminum powder, 5 parts of magnesium powder; 6 parts of acetyl triethyl ...
Embodiment 3
[0033] A deformable solid propellant prepared from the following raw materials: oxidizing agent, reducing agent, shape memory binder, plasticizer and others.
[0034] The oxidant is ammonium perchlorate and ammonium dinitramide; the reducing agent is nano-aluminum powder and magnesium powder; the plasticizer is acetyl triethyl citrate; the shape memory adhesive is an epoxy matrix, a curing agent, and a catalyst And energy-containing additives; wherein the epoxy matrix is bisphenol A epoxy resin, the curing agent is thiocyanuric acid, the catalyst is 2-methylimidazole, the energy-containing additive is polyazide glycidyl ether (GAP), and others are : Alcohol amine complex, aluminate coupling agent, N,N-diphenyl-p-phenylenediamine, carbon black, catocine.
[0035] The mass ratio relationship of each raw material is: 58 parts of ammonium perchlorate, 4 parts of ammonium dinitramide, 12 parts of nano-aluminum powder, 3 parts of magnesium powder; 5 parts of acetyl triethyl citrat...
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