Pre-Phase A Report - Lisa - Nasa
Pre-Phase A Report - Lisa - Nasa
Pre-Phase A Report - Lisa - Nasa
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3.2 The inertial sensor 71<br />
Figure 3.10 Scheme of one channel loop.<br />
to the full scale range of acceleration required for the control of the proof mass. It shall<br />
be changed according to the different operation modes from tens of volts to hundreds of<br />
milli-volts.<br />
A supplementary set of electrodes, called injection electrodes in Figures 3.8, 3.9 and 3.10, is<br />
used to control the proof-mass electrical potential, in particular at the pumping frequency<br />
of the capacitive sensing. This solution has been preferred to a thin gold wire used in<br />
other space accelerometers because of the stiffness and of the damping that the wire may<br />
generate. Experimental investigations have demonstrated that the wire is only compatible<br />
with a resolution of several 10−14 ms−2 / √ Hz at room temperature [86].<br />
3.2.4 Evaluation of performances<br />
The performances of the inertial reference sensor have been evaluated by considering the<br />
geometry and the characteristics of the sensor head, the characteristics of the electronics<br />
configuration and the environment on board the LISA satellite. In particular this last<br />
point leads to a required pressure inside the housing of less than 10−6 Pa.<br />
The evolution of the charge Q of the isolated proof mass is one of the most critical error<br />
sources. On the one hand, the proof mass is subjected to the electrostatic forces appearing<br />
with the image charges on the electrodes in regard to the proof mass; the resultant of<br />
these forces is not null when the configuration is not perfectly symmetric, in particular for<br />
any off-centering of the proof mass with respect to the sensor cage. On the other hand,<br />
this charge Q induces a Lorentz force when it moves in the interplanetary magnetic field.<br />
In fact Q is the sum of the charge acquired when the proof mass separates from the<br />
accelerometer cage at suspension switch-on, and of the charge resulting from the cosmic<br />
particle bombardment, especially from the proton flux over 100 MeV. When considering<br />
achargingrateof10 −17 to 10 −18 C/s [87, 88], the 2×10 −14 C limit required is reached in<br />
less than one hour. Therefore the charge has to be measured exploiting the electrostatic<br />
device itself, and the proof mass has to be discharged, continuously or time by time, for<br />
instance by photo-electric emission induced by ultraviolet light [87].<br />
Other electrostatic-force noises must be considered: they are induced either by the fluc-<br />
Corrected version 2.08 3-3-1999 9:33