DocumentCode :
2931579
Title :
Micro OXCO EWOS-0513: A 20 years space odyssey up to 67P/Churyumov-Gerasimenko
Author :
Guillemot, Philippe ; Cibiel, Gilles ; Richard, Yves ; Tarot, Jean-Marie ; Richard, Guy
Author_Institution :
CNES - French Space Agency, Toulouse, France
fYear :
2015
fDate :
12-16 April 2015
Firstpage :
121
Lastpage :
124
Abstract :
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.
Keywords :
Mars; aerospace instrumentation; celestial mechanics; comets; frequency stability; oscillators; 67P-Churyumov-Gerasimenko comet; CNES; CONSERT instrument; EWOS-0500; French Space Agency; Mars; Rosetta mission; Sojourner rover; frequency stability; low earth orbit; microOXCO EWOS-0513; oscillator; power 150 mW; solar system; space equipment; space industry; space odyssey mission; temperature -30 degC to 60 degC; time 10 year; time 20 year; Life estimation; Oscillators; Qualifications; Satellites; Solar system; Space missions; Space vehicles; ocxo; space applications;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Frequency Control Symposium & the European Frequency and Time Forum (FCS), 2015 Joint Conference of the IEEE International
Conference_Location :
Denver, CO
Print_ISBN :
978-1-4799-8865-5
Type :
conf
DOI :
10.1109/FCS.2015.7138804
Filename :
7138804
Link To Document :
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