CN101376101A - Bitter earth nano-catalyst material capable of being used for high-energy solid propellant and synthetic method thereof - Google Patents

Bitter earth nano-catalyst material capable of being used for high-energy solid propellant and synthetic method thereof Download PDF

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CN101376101A
CN101376101A CN 200710009435 CN200710009435A CN101376101A CN 101376101 A CN101376101 A CN 101376101A CN 200710009435 CN200710009435 CN 200710009435 CN 200710009435 A CN200710009435 A CN 200710009435A CN 101376101 A CN101376101 A CN 101376101A
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solid propellant
nano
temperature
catalyst material
mgo
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CN101376101B (en
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李莉萍
邱晓清
李广社
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Fujian Institute of Research on the Structure of Matter of CAS
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Fujian Institute of Research on the Structure of Matter of CAS
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Abstract

The invention discloses a magnesia nano-catalyst material for a high-energy solid propellant and a synthesis method thereof, and relates to both nano-science and high energy solid propellant fields. The method comprises the steps of dissolving magnesium acetate in absolute alcohol and conducting solvent thermal treatment at the temperature ranging from160 to 20 DEG C to get a magnesic precursor; and placing the precursor into a muffle furnace and conducting calcination at the temperature of 450 DEG C for 2 hours to get white MgO nano-catalyst. The material has a specific surface area of 230m<2>/g and an aperture of 5nm. The temperature of ammonium perchlorate high-temperature decomposition is reduced by 78 DEG C and the apparent heat of decomposition is increased to 1059 J/g from the previous 371J/g.

Description

A kind of bitter earth nano-catalyst material and synthetic method thereof that can be used for high-energy solid propellant
Technical field:
The present invention relates to the high-energy solid propellant field, especially relate to a kind of high-specific surface area MgO nano-catalyst material and synthetic method thereof.
Background technology:
Solid propellant is the power source material of rocket engine, plays an important role in guided missile and space technology development.Ammonium perchlorate (AP) is a high energy oxidizer commonly used in the solid propellant.Its thermal decomposition characteristic has material impact to the combination property of solid propellant.Pure The Thermal Decomposition of Ammonium Perchlorate is divided into low-temperature decomposition and two processes of pyrolytic, and the energy when having limited its burning discharges.In order to improve the combustion speed of composite solidpropellant, need make the interval reach as far as possible of The Thermal Decomposition of Ammonium Perchlorate reaction temperature.Simultaneously,, need to improve the The Thermal Decomposition of Ammonium Perchlorate reaction severity, make it to focus on the release of heat in order to improve the specific impulse value of solid propellant.Adding little amount of catalyst is the effective ways of regulating propellant burning property.Regulate the focus that propellant burning property has become research with nanocatalyst, study the more Nano metal powder (especially aluminium powder) that normally in solid propellant, adds at present.These Nano metal powders are normally to be made by wire (or paper tinsel) electricity consumption explosive method in inert gas (as Ar), and preparation process needs complex apparatus and higher cost.And when propellant burnt in solid engines, the easy fusion of aluminium powder was condensed into aluminium and coagulate drips, and these aluminium drop in the engine usually with fixed attention can not completing combustion, causes performance loss.For this reason, research and development novel nano catalyst, the combination property of raising solid propellant, just particularly important.
The objective of the invention is on the basis of solid propellant present Research of making thorough investigation and study, proposed a kind of new MgO nano-catalyst material that improves the solid propellant performance and preparation method thereof that can be used for.
Studies show that nano-MgO can significantly reduce the high-temperature decomposition temperature of ammonium perchlorate, improve the combustibility of propellant.
Summary of the invention:
The present invention proposes a kind of method of synthesising mesoporous MgO nano-catalyst material, purpose is to prepare Stability Analysis of Structures, high-specific surface area, has good ammonium perchlorate catalytic activity, can develops into the high-energy solid propellant nano catalytic material of new generation that has a extensive future.
The present invention adopts two-step method to prepare the MgO nanocatalyst, and detailed process is as follows: magnesium salts is dissolved in the absolute ethyl alcohol, changes reactor over to behind the formation clear solution, be heated to 140-200 ℃, insulation.After reaction finished, cool to room temperature filtered, and collects, and must contain the presoma of magnesium.Then presoma is calcined in Muffle furnace and obtained the MgO nanocatalyst.
We prepare specific area by above method is 230m 2/ g, the aperture is~5nm MgO mesoporous nano catalyst material.This material has good ammonium perchlorate catalytic activity, can effectively make the high-temperature decomposition temperature of ammonium perchlorate reduce by 78 ℃, the low-temperature decomposition peak almost disappears, and makes two decomposable processes of ammonium perchlorate change a tangible exothermic decomposition into, and apparent heat of decomposition increases to 1059J/g by original 371J/g.
MgO nanocatalyst of the present invention is controlled specific area and the catalytic performance of MgO by accurate control preparation condition; Compare with the nanocatalyst (as Nano metal powder) of existing other structure, MgO nanocatalyst of the present invention has good ammonium perchlorate catalytic activity, and technology of preparing is simple, equipment is less demanding, with low cost.In addition, the HCl reaction that MgO can decompose produce with ammonium perchlorate can effectively reduce solid propellant in use to the pollution of environment.Thereby, have great application prospect in the solid propellant field.
Description of drawings:
Fig. 1 is the stereoscan photograph of MgO.
Fig. 2 a, 2b are respectively nitrogen adsorption-desorption curve and graph of pore diameter distribution thereof of MgO.
Fig. 3 is the DSC curve of MgO catalytic decomposition ammonium perchlorate, a): and pure ammonium perchlorate, b): after adding MgO.
The specific embodiment:
Example 1: the analytically pure magnesium acetate with 4 crystallizations water of 4.29g (0.02mol) is joined in the 150mL absolute ethyl alcohol, and stirring and dissolving obtains clear solution.Then gained solution is transferred in the reactor, sealing places insulating box, 160 ℃ of following insulation 6h, reaction naturally cools to room temperature with reactor after finishing, filter, dry, collect and obtain white precursor samples.Presoma is placed Muffle furnace, calcine 2h down, obtain white MgO nanocatalyst for 450 ℃.
Example 2: the analytically pure magnesium acetate with 4 crystallizations water of 4.29g (0.02mol) is joined in the 150mL absolute ethyl alcohol, and stirring and dissolving obtains clear solution.Then gained solution is transferred in the reactor, sealing places insulating box, 180 ℃ of following insulation 6h, reaction naturally cools to room temperature with reactor after finishing, filter, dry, collect and obtain white precursor samples.Presoma is placed Muffle furnace, calcine 2h down, obtain white MgO nanocatalyst for 450 ℃.
Example 3: on electronic balance, accurately take by weighing the 0.098g ammonium perchlorate, 0.002g MgO nanocatalyst.Both evenly obtain being added with the ammonium perchlorate (content is 2%) of MgO nanocatalyst with the abundant ground and mixed of mortar.Get the pure ammonium perchlorate of 15mg or be added with the ammonium perchlorate of MgO nanocatalyst, place differential scanning calorimeter analysis, comparative study MgO nanocatalyst is to the The Thermal Decomposition of Ammonium Perchlorate catalytic action.

Claims (2)

1, a kind of synthetic method that can be used for the bitter earth nano-catalyst material of high-energy solid propellant is characterized in that: magnesium acetate is dissolved in the absolute ethyl alcohol, and 160-20 ℃ of solvent heat treatment obtains containing the presoma of magnesium; The gained presoma is placed Muffle furnace, calcine 2h down, obtain white MgO nanocatalyst for 450 ℃.
2, a kind of synthetic bitter earth nano-catalyst material of method that adopts claim 1, this material specific area is up to 230m 2/ g, the aperture is~5nm.Can effectively make the high-temperature decomposition temperature of ammonium perchlorate reduce by 78 ℃, apparent heat of decomposition increases to 1059J/g by original 371J/g.
CN 200710009435 2007-08-30 2007-08-30 Bitter earth nano-catalyst material capable of being used for high-energy solid propellant and synthetic method thereof Active CN101376101B (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
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CN102320907A (en) * 2011-08-16 2012-01-18 湖北三江航天江河化工科技有限公司 Method for improving low-temperature mechanical properties of composite solid propellant
CN102343267A (en) * 2011-07-27 2012-02-08 武汉理工大学 Method for preparing carbon-hybridized nickel lithium ferrite nano-catalyst
CN102515984A (en) * 2011-10-14 2012-06-27 华中科技大学 Core-shell nano-composite material and its preparation method
CN101869841B (en) * 2009-04-24 2014-03-05 中国科学院福建物质结构研究所 Ag-Cu-Ni ternary composite metal catalyzing material and synthesis method and application thereof
CN107442095A (en) * 2017-08-25 2017-12-08 哈尔滨工业大学 A kind of preparation method of nano magnesia ozone catalyst and the deep treatment method with its catalysis oxidation coal chemical industrial waste water
CN111599970A (en) * 2020-06-01 2020-08-28 北京化工大学 Magnesium oxide/iron composite material modified diaphragm and preparation method thereof

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CN100357022C (en) * 2005-03-23 2007-12-26 中国石油化工股份有限公司 Load type calcium oxide catalyst, its preparation method and uses
US20070167323A1 (en) * 2006-01-16 2007-07-19 Toda Kogya Corporation Porous carrier for steam-reforming catalysts, steam-reforming catalyst and process for producing reactive mixed gas

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101869841B (en) * 2009-04-24 2014-03-05 中国科学院福建物质结构研究所 Ag-Cu-Ni ternary composite metal catalyzing material and synthesis method and application thereof
CN102343267A (en) * 2011-07-27 2012-02-08 武汉理工大学 Method for preparing carbon-hybridized nickel lithium ferrite nano-catalyst
CN102343267B (en) * 2011-07-27 2012-12-19 武汉理工大学 Method for preparing carbon-hybridized nickel lithium ferrite nano-catalyst
CN102320907A (en) * 2011-08-16 2012-01-18 湖北三江航天江河化工科技有限公司 Method for improving low-temperature mechanical properties of composite solid propellant
CN102320907B (en) * 2011-08-16 2013-09-11 湖北三江航天江河化工科技有限公司 Method for improving low-temperature mechanical properties of composite solid propellant
CN102515984A (en) * 2011-10-14 2012-06-27 华中科技大学 Core-shell nano-composite material and its preparation method
CN102515984B (en) * 2011-10-14 2013-12-25 华中科技大学 Core-shell nano-composite material and its preparation method
CN107442095A (en) * 2017-08-25 2017-12-08 哈尔滨工业大学 A kind of preparation method of nano magnesia ozone catalyst and the deep treatment method with its catalysis oxidation coal chemical industrial waste water
CN111599970A (en) * 2020-06-01 2020-08-28 北京化工大学 Magnesium oxide/iron composite material modified diaphragm and preparation method thereof
CN111599970B (en) * 2020-06-01 2021-06-01 北京化工大学 Magnesium oxide/iron composite material modified diaphragm and preparation method thereof

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