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IRAC Instrument Handbook - IRSA - California Institute of Technology

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<strong>Instrument</strong> Description 13 Electronics<br />

<strong>IRAC</strong> <strong>Instrument</strong> <strong>Handbook</strong><br />

Figure 2.6 : Non-linearity curves for the <strong>IRAC</strong> detectors. The detector responses are fairly linear<br />

until saturation, where there is a steep drop-<strong>of</strong>f in responsivity.<br />

2.4 Electronics<br />

2.4.1 Hardware<br />

<strong>IRAC</strong> has no moving parts (other than the shutter, which was not operated in flight). The instrument takes<br />

data by staring at the sky and sampling the arrays between resets. <strong>IRAC</strong> was capable <strong>of</strong> operating each <strong>of</strong><br />

its four arrays independently and/or simultaneously. All four arrays were used during normal, full-array<br />

operation.<br />

2.4.2 Fowler Sampling<br />

Multiple (Fowler) sampling is used to reduce the effective read noise. This mode <strong>of</strong> sampling consists <strong>of</strong><br />

taking N non-destructive reads immediately after the reset, and another N non-destructive reads near the<br />

end <strong>of</strong> the integration. Differencing is performed in the <strong>IRAC</strong> electronics to generate one integer value<br />

per pixel per exposure to store on the spacecraft and transmit to the ground. The Fowler N used for an

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