Component-based CMDB propellant mechanical prediction method
A technology of propellant and mechanics, applied in special data processing applications, instruments, electrical digital data processing, etc., can solve the problems of model parameter acquisition relying on experimental data, gap between model prediction and actual demand, and insufficient systematic and in-depth research
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[0082] In order to verify the feasibility of the method, the mass fractions of the selected CMDB propellant components are: 50% nitrocellulose NC (12.5% nitrogen content), 32% NG, 10% Octogen HMX, and the remaining additives 8%.
[0083] like figure 1 As shown, a component-based CMDB propellant mechanics prediction method disclosed in this embodiment includes the following steps:
[0084] Step 1: Select and obtain the input parameters of the components according to the atomic group contribution and selection principle table.
[0085] Obtain the molecular degree of freedom N and zero-point binding energy E of the chemical bond by looking up the contribution of the atomic group and the selection principle table coh , and the van der Waals volume V w . According to the principle of superposition, the molecular degree of freedom N=61.3 and the zero-point binding energy E of nitrocellulose NC in CMDB propellant can be respectively determined coh =235070J / mol, and van der Waals...
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