Spheroidic structure high precision vector synthesis nuclear energy micro propulsion system

Abstract

The invention discloses a spheroidic structure high precision vector synthesis nuclear energy micro propulsion system. The spheroidic structure high precision vector synthesis nuclear energy micro propulsion system includes five substructures: a spheroidic vector synthesis support, a nuclear power surface element, a surface element control switch, a surface element heat transfer unit, and a thermoelectric conversion center. The spheroidic structure high precision vector synthesis nuclear energy micro propulsion system uses the particle kinetic energy formed by spontaneous decay of the nucleusto form the recoil power, uses the spheroidic structure to arrange thrust units with different thrust directions, independently and continuously controls each thrust unit through a laminated counter-rotating structure to form a micro propeller in which the magnitude and the direction of the total thrust can be adjusted with high precision, can further convert associated thermal energy of decay into power sources and heat sources to use, and is specifically suitable for precise control and application of a high precision platform with high stability.

Description

technical field [0001] The invention belongs to the technical field of space nuclear energy propulsion, micro-propulsion and vector propulsion. Specifically, the invention relates to a spherical structure with high-precision vector synthesis nuclear energy micro-propulsion. A high-precision vector thrust synthesis propulsion system for synthesizing the football structure, controlling the size and opening and closing state through the face element switch. Background technique [0002] In recent years, with the continuous development of space science and technology and the continuous deepening of space exploration, the types of power sources for space vehicles have gradually become more diverse. Power systems ranging from micronewtons to more than kilonewtons and attitude adjustment systems have emerged in an endless stream. The supporting propulsion devices Many changes and innovations have gradually been produced in continuous practice. [0003] At present, there are many t...

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Problems solved by technology

[0009] The purpose of the present invention is to provide a counter-rotating switch control method based on nuclear energy to adjust the thrust in view of the complexity of the existing attitude adjustment thrust method for space vector propulsion and the lack of additional derotation requirements for the star body. High-precision vector synthesis nuclear energy micro-thruster with quasi-spherical structure that does not change the angular momentum of the star body during the process

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