Nitrine type high-molecular sensitized high-energy ablator, preparation method thereof and target belt made from ablator

A technology of ablation materials and high-energy materials, which is applied in the direction of attacking equipment and compressed gas generation, can solve the problems of large diffusion angle of splashed products, low energy utilization rate, and increased equipment weight, so as to save the glue brushing process, The effect of reducing the weight of working medium and simplifying the production process

Active Publication Date: 2013-05-01
UNIV OF SCI & TECH OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

PVC can meet the use requirements of SAT-21 small satellites and is easy to prepare, but its energy utilization rate is low, the aircraft needs to carry a large amount of working fluid, which increases the weight of the equipment, and there is a problem of excessive outgassing during continuous use, and it contains The diffusion angle of the carbon splash product is too large

Method used

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  • Nitrine type high-molecular sensitized high-energy ablator, preparation method thereof and target belt made from ablator
  • Nitrine type high-molecular sensitized high-energy ablator, preparation method thereof and target belt made from ablator
  • Nitrine type high-molecular sensitized high-energy ablator, preparation method thereof and target belt made from ablator

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0043] Embodiment 1: preparation

[0044] Prepare ablative material in the following proportions:

[0045] Azide materials 79 parts,

[0046] 8 high-energy materials,

[0047] Additives 13 parts.

[0048] (1) Prepare azide-based materials, high-energy materials and additives according to the above proportions, and dissolve them in solvents respectively to obtain azide-based material solutions, high-energy material solutions and additive solutions;

[0049] Wherein, the azide material: 5 g of GAP was dissolved in 20 ml of ethyl acetate.

[0050] Energetic material: 0.51 g of single-base drug was dissolved in 40 ml of ethyl acetate and allowed to stand for 24 hours.

[0051] Additives: 0.5 ml hexamethylene diisocyanate (HDI) dissolved in 5 ml ethyl acetate, 0.01 ml dibutyltin dilaurate (DBTDL), 0.31 g nanocarbon dissolved in 3 ml ethyl acetate.

[0052] (2) Mix the azide material solution obtained in step (1) with the high-energy material solution, and stir evenly;

[0053...

Embodiment 2

[0061] Embodiment 2: preparation

[0062] Prepare ablative material in the following proportions:

[0063] 38 parts of azide materials,

[0064] High energy materials 51 parts,

[0065] Additives 11 parts.

[0066] (1) Prepare azide-based materials, high-energy materials and additives according to the above proportions, and dissolve them in solvents respectively to obtain azide-based material solutions, high-energy material solutions and additive solutions;

[0067] Among them, the azide material: 2.85 g of GAP was dissolved in 20 ml of ethyl acetate.

[0068] Energetic material: 4 g of single-base drug was dissolved in 100 ml of ethyl acetate and allowed to stand for 24 hours.

[0069] Additives: 0.27 ml hexamethylene diisocyanate (HDI) dissolved in 3 ml ethyl acetate, 0.01 ml dibutyltin dilaurate (DBTDL), 0.375 g nanocarbon dissolved in 5 ml ethyl acetate.

[0070] (2) Mix the azide material solution obtained in step (1) with the high-energy material solution, and stir ...

Embodiment 3

[0079] Embodiment 3: preparation

[0080] Prepare ablative material in the following proportions:

[0081] Azide materials 90 parts,

[0082] 70 parts of high-energy materials,

[0083] Additives 15 parts.

[0084] (1) Prepare azide-based materials, high-energy materials and additives according to the above proportions, and dissolve them in solvents respectively to obtain azide-based material solutions, high-energy material solutions and additive solutions;

[0085] Wherein, the azide material: 9 g of GAP was dissolved in 20 ml of ethyl acetate.

[0086] Energetic material: 7 g of single-base drug was dissolved in 55 ml of ethyl acetate and allowed to stand for 24 hours.

[0087] Additives: 5ml hexamethylene diisocyanate (HDI) dissolved in 5ml ethyl acetate, 0.01ml dibutyltin dilaurate (DBTDL), 5g nanocarbon dissolved in 10ml ethyl acetate, 2g CAB381-0.1, 3g TINUVIN328.

[0088] (2) Mix the azide material solution obtained in step (1) with the high-energy material soluti...

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Abstract

The invention provides a nitrine type high-molecular sensitized high-energy ablator which comprises the components by weight part: 5 to 80 parts of nitrine type material, 5 to 70 parts of high energy material and 5 to 15 parts of additive. The invention also provides a preparation method of the ablator and a target belt made from the ablator. According to the invention, an ablative material layer made via the method utilizes the viscous characteristic of the nitrine type high-molecular sensitized high-energy material, integrates the energy of the nitrine type material and the high energy material, and has the advantages of low ablative threshold value, high energy content and viscosity; and the cohesive property between a substrate and the ablator meets the use requirement, and the utilization rate of the laser energy can also meet the use requirement.

Description

technical field [0001] The invention belongs to the technical field of laser propulsion, and in particular relates to an azide polymer sensitized high-energy ablation material, a preparation method thereof, and a target tape prepared by the same. Background technique [0002] Laser micro-propulsion technology can realize the attitude control and orbit maintenance of small satellites. It has the advantages of small impulse bit, light system weight, wide adjustable range of thrust, and no-nozzle structure. alternative status. Due to the weight and energy limitations of small satellites, it is necessary to use a laser with a lower power (≥1W). The etching material must be a polymer material with low thermal conductivity. At present, the target material for laser micro-propulsion is composed of a substrate and an ablation layer. In order to ensure the service life of the thruster, the target material must have a certain length (tens of centimeters to hundreds of meters), width...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C06D5/04C06D5/08
Inventor 焦龙蔡建马宏昊张兴华林谋金沈兆武唐志平
Owner UNIV OF SCI & TECH OF CHINA
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