Charging stable period fast estimating method of composite modification double-base propellant

A double-base propellant and compound modification technology is applied in the fields of rapid estimation of stability during storage, working conditions of explosives, and charge stability of compound-modified double-base propellant, which can solve the problem of difficult to meet chemical stability design and requirements. Evaluate problems such as demand, uneven distribution of stabilizer content, and large amount of aging samples, so as to avoid the manufacturing process of composite modified double-base propellant charge and solve the uneven and uniform distribution of low-content samples

Active Publication Date: 2017-01-04
XIAN MODERN CHEM RES INST
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Problems solved by technology

[0004] Composite modified double-base propellant adopts thermal accelerated aging test to track the effective content of composite stabilizer to obtain the stability period, and commonly used chemical titration (chemical method in which bromine reacts with stabilizer to form bromide) or chromatography to determine the effective content of composite stabilizer As a destructive detection method, the effective content of the composite stabilizer of the pulverized sample is extracted by reflux of ether for 24 hours or longer, and the low boiling point solvent ether is flammable and explosive, and is prepared by mechanically pulverizing the composite modified double-base propellant aging sample The safety of the sample extracted with ether is poor, the operation is cumbersome, time-consuming, and the bromide produced by chemical titration will cause pollution
[0005] For the composite modified double-base propellant material, the law of the effective content of the composite stabilizer of the aging sample obtained by the thermally accelerated aging test at different temperatures, when the stability period is obtained by the Arrhenius equation, because the thermally accelerated aging test adopts at least 4 temperature points (65°C, 75°C, 85°C, 95°C), the number of sampling at each temperat...

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  • Charging stable period fast estimating method of composite modification double-base propellant
  • Charging stable period fast estimating method of composite modification double-base propellant
  • Charging stable period fast estimating method of composite modification double-base propellant

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Embodiment 1

[0082] The typical composite modified double-base propellant GST-1 is taken as a representative for illustration.

[0083] (1) Preparation of near-infrared modeling samples with effective content of compound stabilizer by thermal accelerated aging method

[0084] Typical composite modified double base propellant GST-1 drug cake sandwich structure sample (Φ=30mm, upper tablet 1H1=5mm, sandwich layer 2H2=10mm, lower tablet 3H3=5mm, attached figure 1 ) into a ground-mouth reducing bottle with a capillary exhaust tube (semi-closed condition, attached figure 2 ) at 90°C for accelerated aging, take out the sandwich layer 2 every 2 hours, and obtain composite modified double-base propellant samples with different stabilizer contents, collect 60 samples, and 29 samples (numbered 1-29) are used as internal calibration set for linear fitting and internal cross-validation, and 31 samples as an external validation set (numbered 30-60) for external validation.

[0085] (2) Near-infrared...

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Abstract

The invention relates to a charging stable period fast estimating method of a composite modification double-base propellant. A heat acceleration aging method is used for preparing an model building sample of a composite stabilizing agent effective content near infrared quantitative model in the composite modification double-base propellant; a chemical titration method or a high efficiency liquid chromatography method is used for obtaining the effective content chemical value of the composite stabilizing agents; an near infrared spectrograph collects the spectrograph; the composite stabilizing agent effective content near infrared quantitative model is built through chemometrics; a stable period estimation equation is built by a reliable temperature coefficient r0; the composite stabilizing agent effective content in the single temperature charging column heat acceleration aging process is detected in a tracking way by a near infrared method; the critical time of reaching the critical criterion consumption of the composite stabilizing agent effective content is obtained; the outwards pushing work condition and the stable period at the storage environment temperature are estimated according to the stable period estimation equation. The method has the advantages that the stable period can be obtained only by nondestructively tacking the effective content of different aging time of one charging sample at one temperature by the near infrared method; the sample quantity is reduced by 96 percent; the speed is high; safety and low cost are realized.

Description

technical field [0001] The invention belongs to the technical field of safety evaluation of explosives, and relates to a method for rapidly predicting the working conditions and stability period of explosives during storage. In particular, a near-infrared diffuse reflectance spectrometry is used to detect the effective content of the composite stabilizer of the composite modified double-base propellant single-temperature thermally accelerated aging sample, and the critical time for the effective content of the composite stabilizer to reach the critical criterion is obtained. According to the stability period prediction A method for quickly estimating working conditions and storage stability period of composite modified double-base propellant charge by estimating equation. Background technique [0002] The chemical stability of explosives refers to the ability of explosives to maintain their chemical properties under working conditions and storage conditions without exceeding...

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Application Information

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IPC IPC(8): G01N21/359G01N21/3563G01N30/02G01N31/16
CPCG01N21/3563G01N21/359G01N30/02G01N31/16G01N2021/3572
Inventor 丁黎周静祝艳龙安静杨惠梅
Owner XIAN MODERN CHEM RES INST
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