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
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[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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