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Compact solid-state laser for laser ranging in space high-orbit environment

A solid-state laser, laser ranging technology, applied in solid-state laser parts, lasers, laser parts and other directions, can solve the problems of reducing output energy, laser component damage, large total irradiation dose, etc., to improve work reliability , The effect of improving on-orbit reliability and anti-radiation performance

Active Publication Date: 2019-12-03
BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Vacuum may cause vacuum discharge to damage components, and may also cause non-metallic components to volatilize condensable volatiles, which condense on the film of optical components and cause damage to laser components; weightlessness will cause dust particles inside the optical cavity to be suspended in the optical path, This makes the laser more prone to damage; plasma and high-energy electron irradiation will charge the outer surface of the laser, and then discharge with the electrode of the internal static-sensitive core component Laser Diode Array (LDA), thereby causing breakdown damage; The irradiation of high-energy particles from the sun may modify the laser crystal and Q-switched crystal, thereby reducing the output energy. Especially in the high-orbit environment, the total radiation dose is relatively large, and the above phenomenon is more likely to occur

Method used

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  • Compact solid-state laser for laser ranging in space high-orbit environment
  • Compact solid-state laser for laser ranging in space high-orbit environment
  • Compact solid-state laser for laser ranging in space high-orbit environment

Examples

Experimental program
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Effect test

Embodiment 1

[0053] A compact solid-state laser used for laser ranging in space high-orbit environments, including a laser housing structure 1, a pump module 4 placed in the laser housing structure 1, front cavity mirrors and polarizers placed on both sides of the pump module 4 Component 5, the Q-switching switch component placed on the side of the polarization component 5 away from the pump module 4, the rear cavity mirror placed on the side of the Q-switching switch component away from the polarization component 5, and the rear cavity mirror placed on the laser shell structure 1 close to the front cavity mirror The output window 2, the Q-switching switch driving assembly and the main wave sampling assembly placed on both sides of the laser shell structure 1, and the gas filling valve 9; The interior of the shell structure 1 is inflated.

[0054] The laser housing structure 1 is made of double-layer metal, and the sealing leak rate in the laser housing structure 1 is lower than 10 -8 pa·...

Embodiment 2

[0062] A solid-state laser used in laser ranging in space high-orbit environments. The laser uses a semiconductor laser array to side-pump a rod-shaped laser crystal, and uses an unstable cavity to achieve continuous amplification to output laser light. The solutions of radiation-resistant crystals, structural reinforcement, double-layer metal sealing, vacuum degassing of raw materials, and isolation of photoelectric components are used to avoid the impact of strong radiation, high vacuum, weightlessness and other environmental elements in the space on-orbit environment.

[0063] For the influence of high vacuum and weightlessness on the laser, the technical solution of this embodiment is:

[0064] (1) Double-layer metal seal is used to control the leakage rate below 10 -8 pa·m 3 the s -1 , to avoid vacuum discharge problems during the lifetime.

[0065] (2) Before assembly, during assembly, and after assembly, perform vacuum degassing on parts and raw materials under diffe...

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Abstract

The invention relates to a compact solid-state laser for laser ranging in a space high-orbit environment, which belongs to the technical field of solid-state lasers. Double-layer metal seal is designed to carry out vacuum degassing on components and raw materials in all aspects of installation and adjustment and isolate optical components and electronic components in the laser. The chance of pollution damage, which is caused by high vacuum and weightlessness, of the laser is reduced. Anti-irradiation strengthening is carried out on the laser casing, and electrostatic sensitive devices are effectively isolated. The probability that the laser casing and sensitive devices are damaged due to irradiation charging of plasma and high-energy electrons is reduced. Anti-irradiation laser crystals are used with a structural reinforcement technology to reduce the chance of laser component failure caused by total dose irradiation of high-energy particles. A virtual confocal unstable cavity and a multi-component integrated design technology are used to make the size of the laser highly compact.

Description

technical field [0001] The invention relates to a compact solid-state laser used in space high-orbit environment laser ranging, and belongs to the technical field of solid-state lasers. Background technique [0002] Laser ranging is a technology that enables high-precision distance detection. The detection principle of the laser range finder is to use the laser light source to emit the detection laser to the target, and the photoelectric element receives the laser beam emitted by the target, and the timer measures the time from the emission to the reception of the laser beam, and calculates the distance from the observer to the target. The distance detection accuracy can reach more than 0.1m. [0003] As the laser source of the laser rangefinder, there are semiconductor lasers, fiber lasers, solid-state lasers, etc. For inter-satellite distance detection of 100km, solid-state lasers that can emit high peak power lasers are usually used. A solid-state laser is a laser that ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): H01S3/02H01S3/081H01S3/094H01S3/10H01S3/11H01S3/16H01S3/0941
CPCH01S3/02H01S3/027H01S3/0818H01S3/094H01S3/10061H01S3/11H01S3/1611H01S3/1643
Inventor 颜凡江史文宗杨超李梦龙罗萍萍蒙裴贝桑思晗许春晓王春辉王建永郭元荣雷文平
Owner BEIJING RES INST OF SPATIAL MECHANICAL & ELECTRICAL TECH
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