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A liquid oxygen methane rocket supercharging device and liquid oxygen methane rocket

A liquid oxygen methane and supercharging device technology, which is applied in the direction of rocket engine device, jet propulsion device, container structure installation device, etc., can solve the problems of potential safety hazards and high cost of supercharging device, and achieves improved carrying capacity and low cost. , the effect of reducing quantity or volume

Active Publication Date: 2020-12-22
BEIJING XINGJI RONGYAO SPACE TECH CO LTD +2
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Therefore, the technical problem to be solved by the present invention is to overcome the existing low-temperature and high-pressure gaseous pressurization technology applied to the liquid oxygen methane rocket, the cost of the pressurization device is relatively high, and there are defects in safety hazards, thereby providing a method on the basis of ensuring safety , lower cost liquid oxygen methane rocket booster and liquid oxygen methane rocket

Method used

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  • A liquid oxygen methane rocket supercharging device and liquid oxygen methane rocket
  • A liquid oxygen methane rocket supercharging device and liquid oxygen methane rocket

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Embodiment Construction

[0029] The technical solutions of the present invention will be clearly and completely described below in conjunction with the accompanying drawings. Apparently, the described embodiments are some of the embodiments of the present invention, but not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0030] In addition, the technical features involved in the different embodiments of the present invention described below may be combined with each other as long as there is no conflict with each other.

[0031] Such as figure 1 and 2 A specific implementation of the liquid oxygen methane rocket supercharging device shown, the pressurized gas is cold helium, including a liquid oxygen storage tank 1 and a liquid methane storage tank 2, and liquid oxygen and liquid methane are respectively stored inside. The l...

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Abstract

The invention relates to the technical field of liquid rockets, in particular to a liquid oxygen methane rocket booster device and a liquid oxygen methane rocket. A liquid oxygen methane rocket pressurizing device, comprising: a liquid oxygen storage tank, which is provided with a pressurized gas inlet; Pressurized gas inlet connection. The invention provides a liquid oxygen methane rocket pressurizing device and a liquid oxygen methane rocket with low cost on the basis of ensuring safety.

Description

technical field [0001] The invention relates to the technical field of liquid rockets, in particular to a liquid oxygen methane rocket booster and a liquid oxygen methane rocket. Background technique [0002] Liquid oxygen methane propellant has the characteristics of wide sources, low cost, non-toxic and environmentally friendly, and high performance. It is more suitable for repeated use and the use requirements of low-cost rocket vehicles. It is one of the ideal liquid power options for future space vehicles. At present, many aerospace companies at home and abroad are developing liquid oxygen methane rockets and rocket engines. The pressurization system is used to provide the pressure of the air pillow of the liquid rocket propellant tank. The pressurized gas enters the propellant tank, expands to occupy the space after the propellant is discharged, and generates working pressure on the liquid propellant. On the one hand, it meets the needs of the engine during flight. Th...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F17C1/00F17C7/00F17C13/00F17D1/02F17D3/01F02K9/60F02K9/50
CPCF17C1/00F17C7/00F17C13/002F17D1/02F17D3/01F02K9/605F02K9/50F17C2201/0128F17C2205/013F17C2205/0352F17C2205/0388F17C2221/011F17C2221/017F17C2221/033F17C2223/013F17C2223/0123F17C2225/0123F17C2227/01F17C2227/03F17C2270/0197B64G1/402F05D2260/213
Inventor 彭小波张玺熊宴斌
Owner BEIJING XINGJI RONGYAO SPACE TECH CO LTD
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