Micro OXCO EWOS-0513:一次长达20年的太空漫游,最高可达67P/Churyumov-Gerasimenko

P. Guillemot, G. Cibiel, Yves Richard, J.-M. Tarot, G. Richard
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摘要

这个故事可能始于90年代中期火星上的某个地方,当时“旅居者”探测器证明了用“低成本”系统完成伟大的太空任务是可能的。这是“更好/更快/更便宜”时期的开始。它引导航天机构和航天工业使用“专业”系统而不是完全符合航天标准的系统来开发航天设备。1995年,法国国家空间研究中心(CNES)决定开发一系列“低成本”空间小型化ocxo。一个所谓的EWOS-0500微型OCXO,用于当时的遇险信标,被选中用于此目的。EWOS-0500是一个非常小的尺寸(DIL 14, 1.5 cm3)和低功率(150 mW)的OCXO,在10-11范围内具有短期稳定性(a - dev),在温度范围内的频率稳定性为0.2 ppm[-30°C;+ 60°C)。建立了一个具体的鉴定程序,以演示该OCXO完成空间任务的性能和能力。EWOS-0513微型OCXO诞生。EWOS-513执行了许多太空任务,主要是在近地轨道上。但他们中的一些人也参加了罗塞塔号的任务,进行了为期10年的太阳系之旅,一直到达67P/楚留莫夫-格拉西门科彗星。一旦到达,他们为任务的成功做出了贡献,允许轨道器和着陆器之间的通信,并通过CONSERT仪器参与科学计划。本文重新绘制了该计划的主要步骤和主要性能,该计划最初用于遇险信标的振荡器为罗塞塔号任务的成功做出了贡献。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Micro OXCO EWOS-0513: A 20 years space odyssey up to 67P/Churyumov-Gerasimenko
The story probably started somewhere on the planet Mars in the middle of the 90s' when the Sojourner rover demonstrated that it was possible to make great space missions with `low cost' systems. It was the beginning of the `Better / Faster / Cheaper' period. It led space agencies and space industry to develop space equipment using `professional' systems instead of full space qualified ones. In 1995, the CNES, the French Space Agency, decided to develop a family of `low cost' space miniaturized OCXOs. A so called EWOS-0500 micro OCXO, used up to then for distress beacons, was selected for this purpose. The EWOS-0500 was a very small size (DIL 14, 1.5 cm3) and low power (150 mW) OCXO with a short-term stability in the 10-11 range (A-Dev) and a frequency stability of 0.2 ppm in the temperature range [-30 °C; +60°C]. A specific qualification program was set up, to demonstrate the performances and the capability of this OCXO to fulfil space missions. The EWOS-0513 micro OCXO was born. The EWOS-513 was embarked on numerous space missions, mainly in low earth orbit. But some of them were also embarked on the Rosetta mission for a 10 years journey through the solar system up to the 67P/Churyumov-Gerasimenko comet. Once arrived, they contributed to the success of the mission, allowing telecommunication between the orbiter and the lander and being involved in the science program through the CONSERT instrument. This paper redraws the main steps and the main performances of this program that led an oscillator initially intended for distress beacons to contribute to the success of the Rosetta mission.
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