Imaging sensitivity of a linear interferometer array on lunar orbit

被引:7
|
作者
Shi, Yuan [1 ,2 ]
Xu, Yidong [1 ]
Deng, Li [3 ]
Wu, Fengquan [1 ]
Wu, Lin [3 ]
Huang, Qizhi [1 ]
Zuo, Shifan [4 ,5 ]
Yan, Jingye [3 ]
Chen, Xuelei [1 ,2 ,6 ,7 ]
机构
[1] Chinese Acad Sci, Natl Astron Observ, 20A Datun Rd, Beijing 100101, Peoples R China
[2] Univ Chinese Acad Sci, Sch Astron & Space Sci, Beijing 100049, Peoples R China
[3] Chinese Acad Sci, Natl Space Sci Ctr, Beijing 100190, Peoples R China
[4] Tsinghua Univ, Dept Astron, Beijing 100084, Peoples R China
[5] Tsinghua Univ, Tsinghua Ctr Astrophys, Beijing 100084, Peoples R China
[6] Northeastern Univ, Coll Sci, Dept Phys, Shenyang 110819, Peoples R China
[7] Peking Univ, Ctr High Energy Phys, Beijing 100871, Peoples R China
基金
中国国家自然科学基金;
关键词
instrumentation: interferometers; methods: data analysis; space vehicles: instruments; techniques: interferometric; dark ages; reionization; first stars; radio continuum: general; GALACTIC RADIO-EMISSION; SOUTHERN SKY; 10; MHZ; MODEL; FRAMEWORK; SUMSS;
D O I
10.1093/mnras/stab3623
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
Ground-based observation at frequencies below 30 MHz is hindered by the ionosphere of the Earth and radio frequency interference. To map the sky at these low frequencies, we have proposed the Discovering the Sky at the Longest wavelength mission (DSL, also known as the 'Hongmeng' mission, which means 'Primordial Universe' in Chinese) concept, which employs a linear array of micro-satellites orbiting the Moon. Such an array can make interferometric observations achieving good angular resolutions despite the small size of the antennas. However, it differs from the conventional ground-based interferometer array or even the previous orbital interferometers in many aspects, new data-processing methods need to be developed. In this work, we make a series of simulations to assess the imaging quality and sensitivity of such an array. We start with an input sky model and a simple orbit model, generate mock interferometric visibilities, and then reconstruct the sky map. We consider various observational effects and practical issues, such as the system noise, antenna response, and Moon blockage. Based on the quality of the recovered image, we quantify the imaging capability of the array for different satellite numbers and array configurations. For the first time, we make practical estimates of the point source sensitivity for such a lunar orbit array, and predict the expected number of detectable sources for the mission. Depending on the radio source number distribution which is still very uncertain at these frequencies, the proposed mission can detect 10(2)-10(4) sources during its operation.
引用
收藏
页码:3046 / 3062
页数:17
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