Method for determining starting scheme of catalytic bed of hydrogen peroxide rocket engine

A rocket engine, hydrogen peroxide technology, applied in radiation pyrometry, chemical analysis by catalysis, weighing by removing certain components, etc., can solve problems such as failure to design a start-up plan in a targeted manner

Active Publication Date: 2021-09-10
BEIHANG UNIV
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] In order to solve the problem in the prior art of failing to design a start-up scheme that fully matches the catalytic bed, the purpose of the present invention is to provide a method for determining the start-up scheme of a hydrogen peroxide rocket engine catalytic bed

Method used

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  • Method for determining starting scheme of catalytic bed of hydrogen peroxide rocket engine
  • Method for determining starting scheme of catalytic bed of hydrogen peroxide rocket engine
  • Method for determining starting scheme of catalytic bed of hydrogen peroxide rocket engine

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Embodiment 1

[0058] Please also refer to figure 1 and figure 2 , the present embodiment provides a method for determining the start-up scheme of the catalytic bed of a hydrogen peroxide rocket engine (hereinafter referred to as the "determination method"). For rocket engines that use different concentrations of hydrogen peroxide as the oxidant, it is possible to design a start-up scheme that matches the catalytic bed of the rocket engine in a targeted manner, improve the start-up speed of the catalytic bed, and avoid excessive ignition in the combustion chamber 3 during the ignition stage. Pressure peaks, thereby eliminating the risk of deflagration.

[0059] see image 3 , the rocket engine includes a head cavity 1 , a catalytic bed assembly 2 and a combustion chamber 3 .

[0060] A pressure measuring joint 11 is provided on the side wall of the head cavity 1 . The pressure measuring joint 11 is hollow and tubular and communicates with the inside of the head cavity 1 to facilitate the...

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Abstract

The invention provides a method for determining a starting scheme of a catalytic bed of a hydrogen peroxide rocket engine. The method comprises the steps of carrying out a bubble sheet test, designing a starting time sequence, carrying out a catalytic test, correcting the starting time sequence and obtaining the starting scheme. The decomposition condition of hydrogen peroxide in the rocket engine is simulated by using the bubble sheet test, the starting time sequence is designed for a valve according to the result of the bubble sheet test, a catalytic test is performed in the rocket engine according to the starting time sequence, and then the starting time sequence corresponding to the next group of catalytic tests is corrected according to the result of the catalytic test, so that the starting time sequence is gradually improved. Finally, the last starting time sequence is corrected again and serves as a starting scheme. According to the process, a starting scheme completely matched with the catalytic bed of the rocket engine can be designed in a targeted mode, the starting speed of the catalytic bed is increased, the situation that a combustion chamber in the ignition stage has an over-high ignition pressure peak is avoided, and then the detonation danger is eliminated.

Description

technical field [0001] The invention relates to the field of rocket engines, in particular to a method for determining the start-up scheme of a catalytic bed of a hydrogen peroxide rocket engine. Background technique [0002] As a propellant, hydrogen peroxide has excellent characteristics such as greenness and non-toxicity, so it is widely used in rocket engines, and its main function is to act as an oxidant. At present, a series of studies have been done on the ignition scheme of the rocket engine using hydrogen peroxide as the propellant, and catalytic ignition as one of the ignition schemes has also been widely adopted and widely used. [0003] Compared with other schemes, the catalytic ignition scheme uses a catalytic bed, and liquid hydrogen peroxide is rapidly decomposed into water and oxygen when flowing through the catalytic bed, and is added to the combustion chamber in the gas phase at the outlet of the catalytic bed. Liquid direct injection is more conducive to ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N31/10G01N5/04G01J5/00
CPCG01N31/10G01N5/04G01J5/00G01J2005/0077
Inventor 张源俊辜小明田辉魏天放周闯
Owner BEIHANG UNIV
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