宇宙光学观测试验 1408 碎片

O. Kozhukhov, Y. V. Omelchenko, D. Kozhukhov, O. G. Solomakha, M. V. Kulichenko, O. Shulga, Y. Kozyryev, N. Maigurova
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摘要

由于 2021 年 11 月 15 日俄罗斯反卫星武器的试验,无法运行的 COSMOS 1408 号航天器(NSSDCA/COSPAR ID:1982-092A)被摧毁。这导致产生了大量碎片云,对低地球轨道(LEO)上的其他物体,特别是近轨道物体构成威胁。其中超过 1500 个碎片达到了可追踪的大小。此类事件需要通过所有可用的地面跟踪手段(包括雷达和光学观测)进行快速和即时的监测。以下研究介绍了对乌克兰 COSMOS 1408 所选碎片的光学观测结果。这些观测是 2022 年 2 月由乌克兰国家航天局国家空间设施控制和测试中心的 OES30 望远镜和 "米科拉夫天文台 "研究所的快速机器人望远镜进行的。观测结果表明,在有相对准确的星历数据的情况下,乌克兰光学传感器能够跟踪雷达截面(RCS)小于 0.1 平方米的低地球轨道空间碎片物体。对获取的带有卫星碎片的帧进行了天体测量还原,结果表明,大部分目标物体的轨道参数接近事件发生前原始卫星的轨道参数。此外,处理现有观测数据的结果表明,远地点高度范围大大超过近地点高度范围。这些发现与之前研究人员得出的结论一致。今后,有必要评估传感器观测低地轨道物体毁坏后果的能力,特别是在此类事件发生后的最初几小时和几天内,因为此时可能缺乏精确的碎片轨道数据。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
TEST OPTICAL OBSERVATIONS OF THE COSMOS 1408 FRAGMENTS
The non-functioning spacecraft COSMOS 1408 (NSSDCA/COSPAR ID: 1982-092A) was destroyed as a result of tests involving Russian anti-satellite weapons on 15 November 2021. This led to the creation of a significant debris cloud that poses a threat to other objects in low Earth orbit (LEO), particularly those in close orbits. More than 1500 of these fragments reached trackable sizes. Such events require rapid and immediate monitoring through all available ground tracking means, including radar and optical observation. The following study presents the results of optical observations of the selected fragments of COSMOS 1408 in Ukraine. These observations were carried out by the telescope OES30 from the National Space Facilities Control and Test Center of the State Space Agency of Ukraine and the Fast Robotic Telescope (FRT) of the Research Institute "Mykolaiv Astronomical Observatory" in February 2022. The observations demonstrated that Ukrainian optical sensors are capable of tracking LEO space debris objects with radar cross-sections (RCS) less than 0.1 square meters when relatively accurate ephemeris data is available. The astrometric reduction has been performed for the acquired frames with fragments of the satellite, which revealed that orbital parameters of a significant part of the targeting objects were close to the orbital parameters of the original satellite before the event. Furthermore, the results of processing the available observations indicated that the range of apogee heights significantly exceeds the range of perigee heights. These findings align with conclusions drawn by previous researchers. In the future, it will be essential to assess the capabilities of sensors for observing the aftermath of object destruction in LEO, especially during the initial hours and days following such events when precise debris orbit data may be lacking.
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