Heating gasification device for liquefied gas micro-propulsion system

A gasification device and micro-propulsion technology, which is applied in the directions of jet propulsion device, space flight vehicle propulsion system device, rocket engine device, etc., can solve the problems of high power, waste of energy, etc., and achieves low mass, reduced consumption and simple structure. Effect

Inactive Publication Date: 2011-01-12
BEIHANG UNIV +1
View PDF3 Cites 10 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

But in this way, because the heating device 16 also needs to consume power, the power consumed by the entire liquefied gas micro-propulsion system is relatively large, which wastes energy.

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Heating gasification device for liquefied gas micro-propulsion system
  • Heating gasification device for liquefied gas micro-propulsion system
  • Heating gasification device for liquefied gas micro-propulsion system

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0023] The present invention is a heating gasification device for a liquefied gas micro-propulsion system, comprising a first propellant storage tank 2, a second propellant storage tank 1, a first heat conduction module 5, a second heat conduction module 4, and a pressure reducer 6 , Surge tank 7, safety valve 3, pressure sensor 9 and filter 8, such as figure 2 Shown.

[0024] The first propellant tank 2 and the second propellant tank 1 are used to fill the liquid propellant. The liquid propellant is stored in the first propellant tank 2 and the second propellant tank 1 in liquid form. The stored pressure It is 0.84MPa, the total mass of liquid propellant is 0.6kg, and the mass of liquid propellant can be changed according to different mission requirements. A first heat conduction module 5 and a second heat conduction module 4 are installed on the first propellant tank 2 and the second propellant tank 1, respectively, the propellant inlet of the first heat conduction module 5 a...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The invention discloses a heating gasification device for a liquefied gas micro-propulsion system. The device comprises a first propellant storage box, a second propellant storage box, a first heat conducting module, a second heat conducting module, a pressure reducer, a pressure stabilizing tank, a safety valve, a pressure sensor and a filter. In the device, a passive heating mode is adopted, and a satellite internal heat dissipation unit is used as a heat source, so that extra power consumption is not needed; and the gasification device has the advantages of reducing the production cost, fully gasifying the propellant and ensuring that the propellant completes work in the form of gas state, along with simple structure, a few elements and devices and high reliability and safety.

Description

Technical field [0001] The invention belongs to the technical field of liquefied gas micro-propulsion, and relates to a heating gasification device for a liquefied gas micro-propulsion system. Background technique [0002] As micro-nano satellites are more and more widely used, the liquefied gas micro-propulsion system is widely used on micro-satellites for attitude control and orbit maintenance and control with its unique advantages. Since the propellant is stored in liquid form in the liquefied gas micro-propulsion system, it needs to absorb heat during the gasification process to turn it into gas, and then it is ejected from the thruster of the propulsion system. If the heat absorbed during the gasification process is insufficient , Resulting in incomplete vaporization, part of the propellant will be ejected from the thruster in liquid form, resulting in a decrease in the specific impulse of the propulsion system and a waste of propellant, and may make the propulsion system un...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
Patent Type & Authority Applications(China)
IPC IPC(8): F02K9/42B64G1/40
Inventor 汤海滨訾振鹏晋晓伟蒋建闫志勇邹宇马键
Owner BEIHANG UNIV
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap