Eureka AIR delivers breakthrough ideas for toughest innovation challenges, trusted by R&D personnel around the world.

Laser ablation pulsed plasma thruster

A technology of pulsed plasma and laser ablation, which is applied in the direction of using plasma, thrust reverser, machine/engine, etc., can solve the problems of low energy conversion efficiency, short life of thruster, low utilization rate of working medium, etc., to improve The effect of working fluid utilization, less moving parts, and adjustable power consumption

Active Publication Date: 2016-09-21
NAT UNIV OF DEFENSE TECH
View PDF4 Cites 10 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] Aiming at the problems of short service life, low utilization rate of working medium, low energy conversion efficiency and easy failure of spark plug of pulsed plasma thruster, it provides spacecraft with a thrust output range, high thrust density, high specific impulse and high working medium utilization rate. Laser ablation pulsed plasma thruster with high efficiency, high energy conversion efficiency, simple structure, high reliability and long service life

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
  • Laser ablation pulsed plasma thruster
  • Laser ablation pulsed plasma thruster
  • Laser ablation pulsed plasma thruster

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0043] refer to figure 1 , the present invention provides a laser ablation pulsed plasma thruster, comprising a power processing unit 1, a capacitor unit 2, a transmission line 3, two parallel plates 4 (wherein one parallel plate is an anode, and one parallel plate is a cathode), Working medium supply device 5 , working medium 6 , plume protection device 7 , beam control system 8 , laser 9 , control system 10 , and external magnetic field system 11 .

[0044] The power processing unit is connected to the capacitor unit 2 through a transmission line 3, and the positive and negative output ends of the capacitor unit 2 are respectively connected to the cathode and the anode through a transmission line 3, and the capacitor unit, the transmission line 3, the cathode and the anode form a discharge circuit, and the cathode can be connected to the anode. , Gas ionization and acceleration between the anode, a discharge channel is formed between the cathode and the anode. The power pro...

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 provides a laser ablation pulsed plasma thruster. The laser ablation pulsed plasma thruster comprises a power processing unit, a capacitor unit, a working medium, a working medium supply device, a cathode, an anode and a laser generating mechanism. The power processing unit is connected with the capacitor unit through a transmission line. The positive output end and the negative output end of the capacitor unit are connected to the cathode and the anode through transmission lines correspondingly. The capacitor unit, the transmission lines, the cathode and the anode form a discharging loop, and gas between the cathode and the anode can be ionized and accelerated. A discharging channel is formed between the cathode and the anode. The working medium supply device for fixing and conveying the working medium is arranged at one end of the discharging channel, and the working medium stretches into the discharging channel from the end. Gaps exist between the working medium and the cathode as well as between the working medium and the anode. The laser generating mechanism emits laser beams into the discharging channel to ablate the working medium, the laser beams continuously ablate the working medium to generate part of ionized gas and particulate matters, the ionized gas and the particulate matters enter the discharging channel to form plasma jets moving along the discharging channel, and thrust is generated. The laser ablation pulsed plasma thruster is high in specific impulse, total impulse, working medium utilization rate and control precision.

Description

technical field [0001] The invention relates to an electric propulsion system for spacecraft attitude adjustment, orbit correction, orbit elevation, deep space exploration, manned moon landing, manned landing on Mars and other space missions. In particular, it is an electromagnetically accelerated pulsed plasma thruster that utilizes laser gasification and partial ionization of solid working fluid. Background technique [0002] Solid ablative pulsed plasma thruster (Ablative Pulsed Plasma Thruster, APPT) is an electromagnetically accelerated electric propulsion system. Its principle is to first charge the capacitor to about 2000V, store energy from a few joules to tens of joules, and then use the spark plug to Ignition induces capacitive discharge to generate an arc and ablates the Teflon working fluid through the arc. Finally, the gasified working fluid is further ionized and accelerated under the action of electromagnetic force. The biggest advantage of this kind of thrus...

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
IPC IPC(8): F03H1/00
CPCF03H1/0087
Inventor 何振吴建军张宇李健何兆福张华
Owner NAT UNIV OF DEFENSE TECH
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
Eureka Blog
Learn More
PatSnap group products