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首页> 外文期刊>Planetary and space science >Lunar surface traces of engine jets of Soviet sample return probes: The enigma of the Luna-23 and Luna-24 landing sites
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Lunar surface traces of engine jets of Soviet sample return probes: The enigma of the Luna-23 and Luna-24 landing sites

机译:苏联样本返回探测器的引擎喷气机的月球表面痕迹:Luna-23和Luna-24着陆点的谜团

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We use a photometric method called phase-ratio imaging to study the landing sites of the Soviet Luna-16, Luna-20, Luna-23 and Luna-24 probes using the survey data of the lunar surface, which was carried out with the Narrow-Angle Cameras (NACs) of the Lunar Reconnaissance Orbiter (LRO) spacecraft. The phase-ratio images clearly show diffuse features associated with structure perturbations of the lunar regolith. We suggest that these features are caused by the impact of the gas jets from the rocket engines. The photometric anomalies around the landing sites suggest that the impacts smooth out the surface, destroying the primordial "fairy castle" structure that effectively produces the shadow-hiding effect. The same characteristic features have been found previously for the Apollo spacecraft landings, but over larger spatial scales. The only exception is the landing site of the Luna-24 probe, for which the feature of the possible impact of the gas jets is shifted to the northwest by approximately 150 m. As the Luna-24 descent module worked in the regular mode and could not allow such a shift as the probe was descending vertically, a possible explanation is that the sites of Luna-23 (an unsuccessful sample return mission) and Luna-24 are misidentified. The distance between the sites is about 2 km, which is within the inaccuracy of their coordinate determination. We suggest that because of faulty processing of the radar system for distance/speed control, the incorrectly operated engine and/or thrusters of Luna-23 produced the 150 m lateral drift before final deactivation and hard descent. To better understand the geologic situation, we produce brightness and phase-ratio anaglyphs for the vicinity of the landings.
机译:我们使用一种称为相比成像的光度学方法,使用月球表面的调查数据来研究苏联Luna-16,Luna-20,Luna-23和Luna-24探测器的着陆点-月球侦察轨道飞行器(LRO)的角度照相机(NAC)。相位比图像清楚地显示了与月球巨石结构扰动有关的弥散特征。我们建议这些功能是由火箭发动机的气体喷射的冲击引起的。着陆点周围的光度异常表明,撞击使表面光滑,破坏了原始的“童话城堡”结构,有效地产生了阴影隐藏效果。先前已经为阿波罗号航天器着陆发现了相同的特征,但在更大的空间范围内。唯一的例外是Luna-24探测器的着陆点,其气体射流可能撞击的特征向西北偏移约150 m。由于Luna-24下降模块在常规模式下工作并且由于探头垂直下降而无法进行这种移动,因此可能的解释是Luna-23(不成功的样品返回任务)和Luna-24的位置被错误识别。站点之间的距离约为2 km,这在其坐标确定的准确性之内。我们建议,由于用于距离/速度控制的雷达系统处理不当,Luna-23的发动机和/或推进器操作不当会导致150 m的侧向漂移,然后最终停用和硬下降。为了更好地了解地质情况,我们为着陆区附近生成了亮度和相位比立体图。

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