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 73<br />
sufficient to easily control the proof-mass motion and attitude, in particular when the<br />
drag-free control is not fully operational, at the beginning of the experiment for instance.<br />
A trade-off between these requirements could be obtained with a specific configuration of<br />
the loop electronics that introduces varying control stiffnesses according to the applied<br />
acceleration.<br />
3.2.6 Proof-mass charge control<br />
Charge control of the proof-mass is crucial if spurious electromagnetic forces are to be<br />
kept at a level such that they do not compromise the science goals. As noted earlier the<br />
nominal requirement is to limit the free charge on the proof mass to < 2×10 −14 Cinthe<br />
presence of a continuous charging rate of 10 −17 to 10 −18 C/s [91]. This charge limit comes<br />
from considering the Lorentz force acceleration noise induced in an unshielded charged<br />
proof-mass interacting with the interplanetary magnetic field and it is explained in more<br />
detail in Section 4.2.4. It is conceivable that a factor of up to 100 might be recovered by<br />
shielding provided by the metallic vacuum enclosure around the sensor. Shielding beyond<br />
that level will be very difficult, given the need for access holes in various positions, and<br />
moreover, noise caused by electrostatic interactions of the free charge with the surrounding<br />
electrode structure then becomes significant anyway (see Section 4.2.4).<br />
The baseline charge control technique involves illuminating both the proof mass and its<br />
surrounding electrodes with ultra-violet light to release photoelectrons from both surfaces,<br />
and then to use bias voltages on the electrodes to control the nett transfer of charge. This<br />
technique has been demonstrated already for GP-B [92], albeit at a somewhat higher<br />
level of charge (10−9 C) and much coarser control authority than those required for LISA.<br />
Laboratory tests using 2.5 W low-power mercury discharge lamps of two different types (rf<br />
discharge for GP-B and dc electric discharge for ROSAT [93]) have shown that sufficient<br />
photoelectric emission can be achieved from gold surfaces in both direct and reflected<br />
illumination. The low magnetic susceptibility of the Au/Pt proof-mass alloy unfortunately<br />
results in a particularly high work function and it may be that a gold coating is necessary<br />
on the proof-mass.<br />
The level of bias voltage required to effect sufficient charge control depends on the detailed<br />
electrode geometry, the gaps to be used and the mode of introducing the UV. In the<br />
current scheme, which offers the simplest mechanical solution, the UV will be introduced<br />
onto the central sections of two opposite tranverse faces of the proof-mass. The facing<br />
electrodes will then be illuminated by reflection. This scheme gives a bipolar discharging<br />
capability. However with our current understanding of the charging mechanisms the<br />
belief is that the proof-mass will charge positively and hence the bias voltage will need to<br />
work against the inherent tendancy of this implementation. An alternative scheme which<br />
would avoid the need for significant bias voltages could be to illuminate the electrode and<br />
proof mass with quasi-independently controllable UV fluxes. This is mechanically more<br />
challenging. Laboratory tests are planned to investigate these options further.<br />
There are a number of possible operational modes for the charge control system. One is to<br />
allow the UV to illuminate the proof mass continuously and only rely on the bias voltages<br />
to control the charge. The bias voltage itself would be derived from measurements of<br />
the charge using a dither voltage applied in the transverse direction at a frequency above<br />
Corrected version 2.08 3-3-1999 9:33