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Space Telescope Imaging Spectrograph Instrument Handbook
Space Telescope Science Institute
ACS Instrument Handbook Cycle 19
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Advanced Camera for Surveys Instrument Handbook for Cycle 19 > Chapter 3: Introduction to ACS > 3.3 Instrument Design

3.3 Instrument Design
3.3.1
The ACS channels feature the following detectors:
The WFC employs a mosaic of two 4096 x 2048 Scientific Imaging Technologies (SITe) CCDs. The 15 x 15 µm pixels provide ~0.05 arcseconds/pixel spatial resolution, with critical sampling at 11,600 е, resulting in a nominal 202 x 202 arcsecond field of view (FOV). The spectral sensitivity of the WFC ranges from ~3500 е to ~11,000 е, with a peak efficiency of 48% at ~7000 е (including OTA).
The defunct HRC has a 1024 x 1024 SITe CCD, with 21 x 21 µm pixels that provided ~0.028 x 0.025 arcsecond/pixel spatial resolution with critical sampling at 6300 е. This gave the HRC a nominal 29 x 26 arcsecond field of view. The spectral response of the HRC ranged from ~1700 е to ~11,000 е, and it has a peak efficiency of 29% at ~6500 е (including OTA).
The SBC detector is a solar-blind CsI microchannel plate (MCP) with Multi-Anode Microchannel Array (MAMA) readout. It has 1024 x 1024 pixels, each 25 x 25 µm in size. This provides a spatial resolution of ~0.034 x 0.030 arcseconds/pixels, producing a nominal FOV of 34.6 x 30.1 arcseconds. The SBC UV spectral response ranges from ~1150 е to ~1700 е with a peak efficiency of 7.5% at 1250 е.
The WFC & HRC CCDs
The ACS CCDs are thinned, backside-illuminated full-frame devices cooled by thermo-electric cooler (TEC) stacks housed in sealed, evacuated dewars with fused silica windows. The spectral response of the WFC CCDs is optimized for imaging at visible to near-IR wavelengths, while the HRC CCD spectral response was optimized specifically for near-UV wavelengths. The WFC CCD camera produces a time-integrated image in the ACCUM data-taking mode as did the HRC CCD before January 2007. As with all CCD detectors, there is noise and overhead associated with reading out the detector following an exposure.
The minimum WFC exposure time is 0.5 seconds. The minimum time between successive identical full-frame WFC exposures is 135 seconds. The readout time can be reduced to as little as ~35 seconds for WFC subarrays. The dynamic range for a single exposure is ultimately limited by the depth of the CCD full well (~85,000 efor the WFC and 155,000 e for the HRC), which determines the total amount of charge that can accumulate in any one pixel during an exposure without saturation. Cosmic rays will affect all CCD exposures. CCD observations should be broken into multiple exposures whenever possible to allow removal of cosmic rays in post-observation data processing, see Section 4.3.6.
The SBC MAMA
The SBC MAMA is a photon-counting detector which provides a two-dimensional ultraviolet imaging and spectroscopic capability. It is operated only in ACCUM mode. To protect the MAMA against permanent damage from over-illumination, local and global brightness limits of 50 counts/second/pixel and 200,000 counts/second, respectively are imposed on all SBC targets. Note that the linearity of the MAMA deviates by 1% at a local (pixel) count rate of ~22 counts/second/pixel, which is half the bright object screening limit. The global count rate becomes similarly nonlinear at the screening limit of 200,000 counts/second. More information on the SBC’s nonlinearity and bright object limits is given in Section 4.5, Section 4.6, and Section 7.2, and in ACS ISRs 98-03 and 99-07.
3.3.2
The ACS design incorporates two main optical channels: one for the WFC, and one which is shared by the HRC and SBC. Each channel has independent corrective optics to compensate for spherical aberration in the HST primary mirror. The WFC has silver-coated optics to optimize instrument throughput in the visible and near-IR. The silver coatings cut off at wavelengths shortward of 3500 е. The WFC has two filter wheels which it shared with the HRC, offering the possibility of internal WFC/HRC parallel observing for some filter combinations (Section 7.9). The optical design of the WFC is shown schematically in Figure 3.2. The HRC/SBC optical chain comprises three aluminized mirrors overcoated with MgF2, shown schematically in Figure 3.3. The HRC or SBC channels are selected by means of a plane fold mirror (M3 in Figure 3.3). The HRC was selected by inserting the fold mirror into the optical chain so that the beam was imaged onto the HRC detector through the WFC/HRC filter wheels. The SBC channel is selected by moving the fold mirror out of the beam to yield a two mirror optical chain that focuses light through the SBC filter wheel onto the SBC detector. The aberrated beam coronagraph was accessed by inserting a mechanism into the HRC optical chain. This mechanism positioned a substrate with two occulting spots at the aberrated telescope focal plane and an apodizer at the re-imaged exit pupil. While there was no mechanical reason why the coronagraph could not be used with the SBC, for health and safety reasons, use of the coronagraph was forbidden with the SBC.
Figure 3.2: ACS optical design: wide field channel.
Figure 3.3: ACS optical design: high resolution/solar blind channels
Filter Wheels
ACS has three filter wheels: two shared by the WFC and HRC, and a separate wheel dedicated to the SBC. The WFC/HRC filter wheels contain the major filter sets. Each wheel also contains one clear WFC aperture and one clear HRC aperture (see Chapter 5 for more on filters). Before January 2007, parallel WFC and HRC observations were possible for some filter combinations (auto-parallels). Because the filter wheels were shared, it was not possible to independently select the filter for WFC and HRC parallel observations.
Calibration-Lamp Systems
ACS has a calibration subsystem consisting of tungsten lamps and a deuterium lamp for internally flat fielding each of the optical channels. The calibration lamps illuminates a diffuser on the rear surface of the ACS aperture door, which must be closed for calibration exposures. Under normal circumstances, users are not allowed to use the internal calibration lamps.
In addition, a post-flash capability can mitigate the effects of Charge Transfer Efficiency (CTE) degradation due to progressive radiation damage. Astrometry programs may benefit from this capability, as is discussed briefly in Section 4.3.7.

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