Magnetic propelling device for spacecraft

A propulsion device and spacecraft technology, applied in the direction of aerospace vehicle propulsion system devices, etc., can solve the problems of inability to realize high-thrust magnetic propulsion, complex magnetic moment relationship, etc., and achieve the effect of simple control and simple structure design

Inactive Publication Date: 2015-04-29
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
View PDF7 Cites 9 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The relationship between the magnitude and direction of the thrust of this method and the magnetic moment generated by the conductor ring is complex, and the magnitude of the generated magnetic force is on the order of several micronewtons, which is only equivalent to atmospheric resistance, and cannot achieve magnetic propulsion with greater thrust.

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
  • Magnetic propelling device for spacecraft
  • Magnetic propelling device for spacecraft
  • Magnetic propelling device for spacecraft

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0029] Please refer to Figure 1 to Figure 3 As shown, the magnetic propulsion device of the spacecraft of the present invention includes a base 101, an upper magnetic shielding cavity 102 and a lower magnetic shielding cavity 103 respectively fixed on the upper and lower surfaces of the base 101, and fixed on the upper surface of the base 101 by screws. The upper metal ring 106, the lower metal ring 107 fixed on the lower surface of the base 101, the upper coil 104 and the lower coil 105 respectively located on the upper and lower surfaces of the base 101, the power module 108, and the front and rear sides of the base 101. And the thermal control device 109 that is in direct contact with the base 101 and can cool the base 101 as a whole. The base 101 is a hollow cuboid structure, the upper shielding cavity 102 is fixed at the rear end of the upper surface of the base 101, the lower shielding cavity 103 is fixed at the front end of the lower surface of the base 101, the upper ...

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 magnetic propelling device for a spacecraft. The structural design is simple, the propelling device adopts a strip-shaped coil structure, and a higher total coil current can be generated through multi-circle wire-wrap connection of a low current wire; the direction and size of pushing force can be adjusted along with the direction of the coil and the size of the coil current, the direction of the pushing force is vertical to the direction of the coil current, and the spacecraft adopting the magnetic propelling device disclosed by the invention is simpler to control. Compared with a magnetic moment propelling method, the pushing force in a propelling method of the magnetic propelling device for the spacecraft is higher under the environments of equal current intensity and earth magnetic field; moreover, a plurality of propelling devices can be arranged in an overlapped mode for combined use, so that high pushing force propelling of the spacecraft is realized; when the propelling device works, a magnetic field is generated around, space charged particles are deflected under the effect of the magnetic field when getting close to the spacecraft, and the device has certain shielding and protecting effects on the space charged particles for the spacecraft; moreover, the magnetic moment sizes of the propelling devices counteract with each other, and no extract magnetic moment effect is generated for the spacecraft.

Description

Technical field: [0001] The invention relates to a spacecraft magnetic propulsion device, which belongs to the field of spacecraft propulsion systems. Background technique: [0002] The conventional jet propulsion device of spacecraft needs to continuously consume fuel, which restricts its service life and the life of the spacecraft, and at the same time increases the initial launch weight of the spacecraft, thereby increasing the cost of rocket launch and the cost of spacecraft use. Therefore, the propulsion method and device without fuel consumption is one of the main goals in the field of current spacecraft propulsion technology. [0003] At present, the research on propulsion methods for spacecraft without fuel consumption mainly focuses on three directions: electrostatic propulsion, electric tethered propulsion and magnetic propulsion. [0004] The electrostatic propulsion method makes the spacecraft whole with positive or negative charge through space plasma charging ...

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): B64G1/40
Inventor 全荣辉程世豪许猛高著秀方美华黄朝艳王志强
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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