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| Format: | Preprint |
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2025
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| Online Access: | https://arxiv.org/abs/2507.16317 |
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| _version_ | 1866912730172096512 |
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| author | Hong, Xiaoyu Wu, Weiren Liu, Qinghui Yu, Dengyun Wang, Chi Shuai, Tao Zhong, Weiye Zhu, Renjie Xie, Yonghui Zhang, Lihua Xiong, Liang Tang, Yuhua Zou, Yongliao Li, Haitao Wang, Guangli Xie, Jianfeng Xue, Changbin Geng, Hao Zhang, Juan Wu, Xiaojing Huang, Yong Zheng, Weimin Liu, Lei Wu, Fang Zhang, Xiuzhong An, Tao Yang, Xiaolong Tong, Fengxian Gurvits, Leonid I. Zheng, Yong Gu, Minfeng Ma, Xiaofei Li, Liang Li, Peijia Zhao, Shanshan Rui, Ping Chen, Luojing Chen, Guohui Li, Ke Zhang, Chao Liu, Yuanqi Jiang, Yongchen Wang, Jinqing Wang, Wenbin Sun, Yan Hao, Longfei Cui, Lang Jiang, Dongrong Qian, Zhihan Ye, Shuhua |
| author_facet | Hong, Xiaoyu Wu, Weiren Liu, Qinghui Yu, Dengyun Wang, Chi Shuai, Tao Zhong, Weiye Zhu, Renjie Xie, Yonghui Zhang, Lihua Xiong, Liang Tang, Yuhua Zou, Yongliao Li, Haitao Wang, Guangli Xie, Jianfeng Xue, Changbin Geng, Hao Zhang, Juan Wu, Xiaojing Huang, Yong Zheng, Weimin Liu, Lei Wu, Fang Zhang, Xiuzhong An, Tao Yang, Xiaolong Tong, Fengxian Gurvits, Leonid I. Zheng, Yong Gu, Minfeng Ma, Xiaofei Li, Liang Li, Peijia Zhao, Shanshan Rui, Ping Chen, Luojing Chen, Guohui Li, Ke Zhang, Chao Liu, Yuanqi Jiang, Yongchen Wang, Jinqing Wang, Wenbin Sun, Yan Hao, Longfei Cui, Lang Jiang, Dongrong Qian, Zhihan Ye, Shuhua |
| contents | The Lunar Orbital VLBI Experiment (LOVEX) is a scientific component of the Chinese Lunar Exploration Project (CLEP) Chang'E-7. The spaceborne component of LOVEX is implemented onboard the relay satellite QueQiao-2, which was launched on 2024 March 20, and later placed into an elliptical selenocentric orbit. The LOVEX-specific payload consists of an X-band cryogenic receiver, a hydrogen maser frequency standard, and VLBI data formatting and acquisition electronics. Several components of the QueQiao-2 nominal onboard instrumentation, such as the 4.2-meter antenna, the data storage device, and the downlink communication system, contribute to the overall spaceborne VLBI instrumentation. This allows us to form a space radio telescope capable of co-observing with Earth-based radio telescopes in VLBI mode. In this space VLBI system, the length of the baseline extends up to approximately 380,000 km. This paper presents the LOVEX scientific objectives, architecture, instrumentation, pre-launch tests, in-flight verification and calibration, and the first in-flight detections of interferometric response (''fringes'') achieved through observations of the quasar AO 0235+164 and the Chang'E-6 orbital module, positioned at the Sun-Earth Lagrange point L2. These initial results demonstrate the successful performance of LOVEX, verifying its capability for both astronomical and spacecraft tracking observations at ultra-long VLBI baselines. |
| format | Preprint |
| id |
arxiv_https___arxiv_org_abs_2507_16317 |
| institution | arXiv |
| publishDate | 2025 |
| record_format | arxiv |
| spellingShingle | Lunar Orbital VLBI Experiment: motivation, scientific purposes and status Hong, Xiaoyu Wu, Weiren Liu, Qinghui Yu, Dengyun Wang, Chi Shuai, Tao Zhong, Weiye Zhu, Renjie Xie, Yonghui Zhang, Lihua Xiong, Liang Tang, Yuhua Zou, Yongliao Li, Haitao Wang, Guangli Xie, Jianfeng Xue, Changbin Geng, Hao Zhang, Juan Wu, Xiaojing Huang, Yong Zheng, Weimin Liu, Lei Wu, Fang Zhang, Xiuzhong An, Tao Yang, Xiaolong Tong, Fengxian Gurvits, Leonid I. Zheng, Yong Gu, Minfeng Ma, Xiaofei Li, Liang Li, Peijia Zhao, Shanshan Rui, Ping Chen, Luojing Chen, Guohui Li, Ke Zhang, Chao Liu, Yuanqi Jiang, Yongchen Wang, Jinqing Wang, Wenbin Sun, Yan Hao, Longfei Cui, Lang Jiang, Dongrong Qian, Zhihan Ye, Shuhua Instrumentation and Methods for Astrophysics The Lunar Orbital VLBI Experiment (LOVEX) is a scientific component of the Chinese Lunar Exploration Project (CLEP) Chang'E-7. The spaceborne component of LOVEX is implemented onboard the relay satellite QueQiao-2, which was launched on 2024 March 20, and later placed into an elliptical selenocentric orbit. The LOVEX-specific payload consists of an X-band cryogenic receiver, a hydrogen maser frequency standard, and VLBI data formatting and acquisition electronics. Several components of the QueQiao-2 nominal onboard instrumentation, such as the 4.2-meter antenna, the data storage device, and the downlink communication system, contribute to the overall spaceborne VLBI instrumentation. This allows us to form a space radio telescope capable of co-observing with Earth-based radio telescopes in VLBI mode. In this space VLBI system, the length of the baseline extends up to approximately 380,000 km. This paper presents the LOVEX scientific objectives, architecture, instrumentation, pre-launch tests, in-flight verification and calibration, and the first in-flight detections of interferometric response (''fringes'') achieved through observations of the quasar AO 0235+164 and the Chang'E-6 orbital module, positioned at the Sun-Earth Lagrange point L2. These initial results demonstrate the successful performance of LOVEX, verifying its capability for both astronomical and spacecraft tracking observations at ultra-long VLBI baselines. |
| title | Lunar Orbital VLBI Experiment: motivation, scientific purposes and status |
| topic | Instrumentation and Methods for Astrophysics |
| url | https://arxiv.org/abs/2507.16317 |