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Water-based propulsion system and method applied to high orbit satellite

A high-orbit satellite and propulsion system technology, which is applied to the propulsion system devices of space navigation aircraft, space navigation equipment, space navigation aircraft and other directions to achieve the effect of improving practicability

Active Publication Date: 2019-08-16
BEIJING INST OF CONTROL ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0008] The technical problem solved by the present invention is: to overcome the deficiencies of the prior art, to provide a water-based propulsion system and method applied to high-orbit satellites, to solve the engineering practicability of the water-based propulsion system in high-orbit satellites, to make the high-orbit Orbital satellite propulsion specific impulse can reach more than 360s

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  • Water-based propulsion system and method applied to high orbit satellite
  • Water-based propulsion system and method applied to high orbit satellite

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Embodiment Construction

[0027] Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. Although exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited by the embodiments set forth herein. Rather, these embodiments are provided for more thorough understanding of the present disclosure and to fully convey the scope of the present disclosure to those skilled in the art. It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0028] The invention proposes a water-based propulsion system applied to high-orbit satellites, including a power supply, a water tank, a static water supply ...

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Abstract

The invention discloses a water-based propulsion system and method applied to a high orbit satellite. The water-based propulsion system comprises a power source, a water tank, a static water supply proton exchange membrane electrolysis tank, a hydrogen and oxygen management system, a hecto-Newton scale gaseous hydrogen gaseous oxygen track control engine, and a Newton scale gaseous hydrogen gaseous oxygen attitude control engine. According to the water-based propulsion system and method applied to the high orbit satellite, the problems that hydrogen and oxygen gases are difficult to be managedon a long-term basis in the space environment and that the hydrogen and oxygen gases with an equivalent mixing ratio are difficult to be efficiently utilized are solved, and engineering practicability of a hydrogen and oxygen propulsion system in a space flight platform is improved.

Description

technical field [0001] The invention belongs to the field of space propulsion technology, and in particular relates to a water-based propulsion system and method applied to high-orbit satellites. Background technique [0002] Hydrogen-oxygen propulsion is currently the chemical propulsion form with the highest specific impulse. [0003] Water-based propulsion technology is a space propulsion technology based on proton exchange membrane water electrolysis cell (SPE), space gas hydrogen-oxygen engine and hydrogen arc thruster. This technology produces hydrogen and oxygen gas through electrolysis of water and supplies it to the engine to generate thrust. This technology allows the space flight platform to generate a chemical thrust with a specific impulse of more than 360s in orbit only by carrying low-pressure water. It has the characteristics of high specific impulse, green and pollution-free, safe storage, and low cost, and meets the requirements of current space missions f...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/40
CPCB64G1/402
Inventor 林震尹文娟唐飞王猛杰宋涛焦焱李泽
Owner BEIJING INST OF CONTROL ENG
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