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中国物理学会期刊

中国空间站冷原子光钟激光系统

CSTR: 32037.14.aps.72.20230412

Laser system of cold atom optical clock in China Space Station

CSTR: 32037.14.aps.72.20230412
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  • 中国研制的世界首台空间冷原子光钟于2022年10月31日随“梦天”实验舱成功发射, 进入中国空间站. 紧凑稳定的激光系统是实现光钟空间应用的关键环节. 本课题组提出类同步调谐方案, 研制了高性能外腔半导体激光器, 能同时满足空间光钟对激光器调谐范围、线宽和力学热学稳定性的要求. 采用注入锁定和锥形放大器进行激光功率放大, 满足了空间光钟对激光功率的要求. 本文简要介绍了空间冷原子光钟的系统构成、激光器方案和电控系统, 并对光钟激光系统面临的问题和发展方向进行了总结和展望.

     

    The world's first space optical clock (SOC) developed in China, which is composed of five subsystems, i.e. an optical unit, a physics unit, an electronic control unit, a space optical frequency comb, and an ultrastable laser, was successfully launched with the Mengtian space laboratory on October 31, 2022, and entered into the China Space Station (CSS). Compact and stable laser is a key element for the operation of the SOC. The optical unit consists of 5 lasers with wavelengths of 461, 679, 689, 707 and 813 nm, respectively. With a synchronous-tuning-like scheme, high-quality external cavity diode lasers (ECDLs) are developed as the seeds. The linewidths of the lasers are all reduced to approximately 100 kHz, and their tuning ranges, free from mode hopping, are capable of reaching 20 GHz, satisfying the requirements for the SOC. With careful mechanical and thermal design, the stability of the laser against vibration and temperature fluctuation is sufficiently promoted to confront the challenge of rocket launching. While the power from the ECDL is sufficient for 679-nm repump laser and 707-nm repump laser, additional injection lock is utilized for the 461-nm laser and 689-nm laser to amplify the power of the seeds to more than 600 mW, so that effective first and second stage Doppler cooling can be achieved. To generate an optical lattice with deep enough potential well, over 800-mW 813-nm lasers are required. Therefore, a semiconductor tapered amplifier is adopted to amplify the seed to more than 2 W, so as to cope with various losses of the coupling optics. The wavelengths and output power values of the 5 lasers are monitored and feedback is controlled by the electronic control unit. All the modules are designed and prepared as orbital replaceable units, which can be easily replaced by astronauts in case failure occurs. Now the lasers are all turned on and operate normally in CSS. More data of the SOC will be obtained in the near future. At present stage, according to our evaluation, the continuous operation time of the SOC is limited by the injection locked lasers, which are relatively vulnerable to mode hopping. Hopefully, this problem can be solved by improving the laser diode preparing technology, or developing fiber lasers with compact frequency conversion modules.

     

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