A kind of high density specific impulse propellant and preparation method thereof
A high-density, propellant technology, used in offensive equipment, explosives, compressed gas generation, etc., can solve problems such as difficulty in improving the energy performance of formulations, inability to use propellants for high-energy density materials, and achieve process cost and preparation time. Reduced, improved quality controllability, good safety effects
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preparation example Construction
[0046] The preparation method of the above-mentioned high-density specific impulse propellant, comprising the following steps:
[0047] (1) Using the laser selective melting and forming method, the metal fuel is printed into the skeleton of the three-dimensional space lattice structure;
[0048] (2) make the adhesive and the oxidant into a paste-like material;
[0049] (3) adding the paste-like material obtained in the step (2) into the skeleton cavity of the three-dimensional space lattice structure obtained in the step (1), and pressing it into a dense and uniform whole to obtain a high-density specific impulse propellant.
[0050] Further, in step (1), the laser selective melting forming printing conditions are: laser power 200-400W, scanning speed 600-1200mm / s, scanning spacing 0.05-0.1mm, scanning layer thickness 0.03-0.05mm.
[0051] Further, in step (2), the method that binder and oxidant are made into dough-like material is:
[0052] (21) Soak the binder in the solve...
Embodiment 1
[0057] Table 1 embodiment 1 high density specific impulse propellant formula
[0058] Recipe composition Mass percentage content (%) Metal fuel (aluminum-based alloy powder) 25 Oxidizer (CL-20) 70 Binder (ethylene-vinyl acetate copolymer) 5
[0059] Table 2 Properties of the propellant obtained in Example 1
[0060] Density / (g / cm 3 )
Embodiment 2
[0062] Table 3 embodiment 2 high density specific impulse propellant formula
[0063] Recipe composition Mass percentage content (%) Metal fuel (aluminum-based alloy powder) 30 Oxidizer (AP) 67 Binder (68# wax) 3
[0064] The propellant properties obtained in Table 4 Example 2
[0065] Density / (g / cm 3 )
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