Electrostatic space accelerometers for present and future missions

被引:76
|
作者
Touboul, P [1 ]
Foulon, B [1 ]
Willemenot, E [1 ]
机构
[1] Off Natl Etud & Rech Aerosp, F-92322 Chatillon, France
关键词
D O I
10.1016/S0094-5765(99)00132-0
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Numerous space applications have required to dale, dedicated accelerometers with ranges and sensitivities optimised for the in-orbit environment. In microgravity applications, the vibration levels of the platforms carrying experiments have to be surveyed or controlled. In Earth observation, the drag measurement of the satellites improves the accuracy of the low orbit recovery. The accelerometers can also participate in a drag compensation system or constitute a gradiometer aiming at the fine determination of the Earth's gravity field exploiting resolution of 0.1 pg. In the field of Fundamental Physics, European and American projects require even higher sensitivities in the low frequency domain between 10(-4) and 10(-2) Hz. In view of these applications, dedicated accelerometers are being developed, all based on the electrostatic suspension of a proof-mass. From the experience acquired from the GRADIO accelerometer development dedicated to space gradiometry (late 80 s), the accelerometer ASTRE has been realised and delivered to ESA for the monitoring of the SPACELAB microgravity environment during the STS-78 shuttle flight in June 96. Cryogenic differential accelerometers are being developed for the in-orbit test of the Equivalence Principle with an accuracy of 10(-17) objective of the GEOSTEP mission studied by CNES. (C) 2000 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:605 / 617
页数:13
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