Imaging sensitivity of a linear interferometer array on lunar orbit

Author:

Shi Yuan12,Xu Yidong1ORCID,Deng Li3,Wu Fengquan1,Wu Lin3,Huang Qizhi1,Zuo Shifan4,Yan Jingye3,Chen Xuelei1256

Affiliation:

1. National Astronomical Observatories, Chinese Academy of Sciences, 20A Datun Road, Beijing 100101, P. R. China

2. University of Chinese Academy of Sciences, School of Astronomy and Space Science, Beijing 100049, P. R. China

3. National Space Science Center, Chinese Academy of Sciences, Beijing 100190, P. R. China

4. Department of Astronomy and Tsinghua Center for Astrophysics, Tsinghua University, Beijing 100084, P. R. China

5. Department of Physics, College of Sciences, Northeastern University, Shenyang 110819, China

6. Center of High Energy Physics, Peking University, Beijing 100871, P. R. China

Abstract

ABSTRACT 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 102–104 sources during its operation.

Funder

Chinese Academy of Sciences

National Natural Science Foundation of China

National Key Research and Development Program of China

Ministry of Science and Technology

CAS

Publisher

Oxford University Press (OUP)

Subject

Space and Planetary Science,Astronomy and Astrophysics

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