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A kind of high-strength butylated hydroxy propellant and preparation method thereof

A butylated hydroxy propellant, high-strength technology, used in offensive equipment, non-explosive/non-thermal agent components, explosives, etc. Small impact, improved strength, simple preparation effect

Active Publication Date: 2021-06-22
HUBEI INST OF AEROSPACE CHEMOTECHNOLOGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to overcome the defects of poor slurry process performance, poor pourability, poor adjustment of burning rate and low elongation of high-strength hydroxybutyl propellant in the prior art, and provide a high-strength hydroxybutyl propellant The propellant has the characteristics of high strength, high elongation, wide adjustable range of burning rate, excellent process performance, and simple preparation, and its preparation method is provided. Through the improvement of the preparation method, its strength performance can be further improved

Method used

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  • A kind of high-strength butylated hydroxy propellant and preparation method thereof
  • A kind of high-strength butylated hydroxy propellant and preparation method thereof
  • A kind of high-strength butylated hydroxy propellant and preparation method thereof

Examples

Experimental program
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Effect test

Embodiment 1

[0036] A high-strength butylated hydroxyl propellant and a preparation method thereof mainly comprise the following process steps:

[0037] Step (1), take the raw material according to the following mass percentage content:

[0038] 6.934% HTPB, 0.2% MAPO, 3.58% DOS, 5% AL, 10% RDX, 73.5% AP;

[0039] Step (2), mixing the raw materials described in step (1) uniformly at 60°C;

[0040] Step (3), weighing 0.586% IPDI and adding it to the mixture made in step (2) to continue mixing under vacuum at 60°C for 60min;

[0041] Step (4), weighing 0.2% vinylcyclohexene diepoxide and adding it to the mixture made in step (3) and continuing vacuum mixing at 60° C. for 15 minutes to make propellant slurry;

[0042] Step (5), the propellant slurry prepared in step (4) is poured into the engine casing or various molds using a vacuum pouring system, and cured in an oven at 70°C for 96 hours to obtain a high-strength butylated hydroxyl propellant.

[0043] The mechanical properties of the p...

Embodiment 2

[0047] A high-strength butylated hydroxyl propellant and a preparation method thereof mainly comprise the following process steps:

[0048] Step (1), take the raw material according to the following mass percentage content:

[0049]7.599% HTPB, 0.2% MAPO, 3.0% DOS, 18% AL, 70.5% AP;

[0050] Step (2), mixing the raw materials described in step (1) uniformly at 60°C;

[0051] Step (3), weighing 0.561% IPDI and adding it to the mixture made in step (2) to continue mixing under vacuum at 60°C for 50min;

[0052] Step (4), weighing 0.14% DMTDA and adding it to the mixture made in step (3) and continuing vacuum mixing at 60° C. for 20 minutes to make propellant slurry;

[0053] Step (5), the propellant slurry prepared in step (4) is poured into the engine casing or various molds using a vacuum pouring system, and cured in an oven at 60°C for 192 hours to obtain a high-strength butylated hydroxyl propellant.

[0054] Table 2 shows the effect of reinforcing agent addition sequence...

Embodiment 3

[0058] A high-strength butylated hydroxyl propellant and a preparation method thereof mainly comprise the following process steps:

[0059] Step (1), take the raw material according to the following mass percentage content:

[0060] 7.045% HTPB, 0.25% MAPO, 3.83% DOS, 9.6% AL, 15% RDX, 63.7% AP;

[0061] Step (2), mixing the raw materials described in step (1) uniformly at 50°C;

[0062] Step (3), weighing 0.475% TDI and adding it to the mixture prepared in step (2) to continue mixing under vacuum at 50°C for 45min;

[0063] Step (4), weighing 0.1% N,N-dihydroxyisopropylaniline and adding it to the mixture prepared in step (3), and continuing to vacuum mix at 50° C. for 10 minutes to prepare a propellant slurry;

[0064] Step (5), the propellant slurry prepared in step (4) is poured into the engine casing or various molds using a vacuum pouring system, and cured in an oven at 50°C for 168 hours to obtain a high-strength hydroxybutyl propellant.

[0065] The mechanical prope...

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Abstract

Provided is a high-strength butylated-hydroxyl propellant and a preparation method thereof. The high-strength butylated-hydroxyl propellant is based on a conventional butylated-hydroxyl propellant by adding a reinforcing agent and optimizing the formula so that it has high strength, high elongation, The adjustable range of burning rate is wide, the process performance is excellent, and the preparation is simple; in terms of the preparation method, the mechanical properties of the propellant are further improved by optimizing the order of adding the reinforcing agent. Various high-performance strategic and tactical missile solid motors required.

Description

technical field [0001] The invention generally belongs to the technical field of propellants, and in particular relates to a high-strength butylated hydroxyl propellant and a preparation method thereof. Background technique [0002] Hydroxybutylene propellant has been widely used in various solid rocket motor charges. Solid propellant grains must be able to withstand tests such as thermal cycling, broadband vibration, ignition pressure effects, and loading environments, otherwise catastrophic failure of the engine may result. With the rapid development of military technology, various high-performance strategic and tactical missile solid motors have put forward higher requirements for propellant performance. Especially for the free-loading grain engine, considering that the deformation of the grain due to storage and flight overload will affect the air passage in the inner flow field and cause the engine to explode, a high-strength propellant is required to meet the applicat...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C06B25/34C06B25/40C06B23/00C06D5/06
CPCC06B23/00C06B23/009C06B25/34C06B25/40C06D5/06
Inventor 葛志强程新丽吉志强李忠友姚南陈炉洋吴世曦周重洋
Owner HUBEI INST OF AEROSPACE CHEMOTECHNOLOGY