At launch in 1997, the median dark rate (excluding hot pixels) for the STIS CCD was about 0.0015 e
−/s. The on-orbit environment causes radiation damage which, over time, increases both the dark current and the number of hot pixels. The CCD is annealed once every four weeks by turning of the thermo-electric cooler (TEC) which allows the CCD to warm from its usual operating temperature near
−83 C to approximately +5 C. While this slows the effects of radiation damage it does not eliminate it. By the time that the STIS Side-1 electronics failed in May 2002, the median dark rate had increased to about 0.004 e
−/s.
As the Side-2 electronics lack a working temperature sensor at the detector itself, the CCD can no longer be maintained at a fixed temperature, and this causes both the temperature of the CCD chip and the dark current to vary as the temperature of the HST aft-shroud environment into which the STIS CCD TEC radiates heat changes. This leads to fluctuations of the CCD dark current on short time scales as HST changes its orientation with respect to the Sun and Earth and moves in and out of the Earth’s shadow, as well as on longer time scales where the heat input can vary due to the seasonal change of the Earth’s distance from the Sun, the degradation of HST’s thermal insulation, and the heat inputs from other HST instruments. While the CCD detector temperature can no longer be directly measured, it has been shown that the temperature of the CCD housing (available in the telemetry value
OCCDHTAV) can be used as a surrogate for the detector temperature. The dark current is observed to increase by about 7% for each degree increase in the housing temperature (see
STIS ISR 2001-03 for additional details).
The combination of radiation damage and the resulting loss of charge transfer efficiency (
Section 7.3.7), also results in a dark current that is no longer distributed uniformly over the detector. The effective dark current is much lower near the top of the detector, close to the readout register. This provides another reason to utilize the E1 aperture positions when observing faint objects (see
“Mitigation of CTE Loss for Long-Slit Spectroscopy” ). The trend for the dark current both at the center of the detector and near the top of the chip at the E1 aperture positions is shown in
Figure 7.8. In this figure, all measured dark values have been scaled to a CCD housing temperature of 22 C, which is typical of values observed during September 2009. We expect that the CCD dark current will continue to increase with time. For use in the STIS ETC for Cycle 18, we have adopted a dark current of 0.015 e
− s
−1; this value is a compromise between the values expected at the detector center and near the E1 position during mid-2011.
There are no hard bright object limits to worry about for CCD observations, because the CCD cannot be damaged by observations of bright sources. However, the CCD pixels do saturate at high accumulated count levels, due to the finite depth of the CCD full well. The CCD saturates at ~144,000 electrons pixel
−1 in most of the effective area of the chip; however, over the outermost (serial=x) portion the CCD saturates at 120,000 electrons pixel
−1. The variation of the CCD full well over the chip occurs because of nonuniformity in the process of boron implantation, which creates the potential wells in this type of CCD. Accumulations up to the full well limit can be observed only in the
CCDGAIN=4 setting, as the gain amplifier already saturates at ~33,000 electrons pixel
−1 in the
CCDGAIN=1 setting (see
Section 7.2.10).
Saturation imposes a limit on the product of the count rate and the integration time. Keep the total counts
in the pixels of interest below the saturation level, either by keeping the exposure time short enough that the limit is not violated in any single integration or by choosing a more appropriate configuration. You can allow saturation to occur in regions of the image over which you do not wish to extract information (e.g., you can allow a star or single emission line to saturate if you are interested in other features). Remember, however, that once the CCD well is over full, charge will bleed along the columns of the CCD so that neighboring pixels (along the slit for spectroscopic observations) will also be affected. Saturation
cannot be corrected in post-observation data processing.
An interesting exception to this is described in Gilliland, Goudfrooij & Kimble, 1999,
PASP,
111, 1009. For
CCDGAIN=4 the response remains linear up to, and even far beyond saturation if one integrates over the pixels receiving the charge bleed. Because the bleeding is perpendicular to the dispersion direction, for point sources such saturation does not compromise spectral purity. Signal to noise values of ~10,000 have been demonstrated for saturated data (see
STIS ISR 1999-05 for a time series application and Bohlin & Gilliland, 2004,
AJ 127, 3508 for a measurement of Vega’s absolute flux).
In Section 6.2, we explained how to determine the peak counts sec
−1 pixel
−1 expected for your observation. In
Chapter 13 for each spectroscopic mode and in
Chapter 14 for each imaging mode, we provide plots of exposure time to fill the CCD well versus source flux for each STIS configuration. Lastly,
exposure time calculators are available on the STScI STIS Web site. Use one of these sources to ensure that your observations will not saturate sources of interest.
The STIS CCD camera features a high-speed shutter that eliminates the need for a shutter illumination correction, even at the shortest commandable exposure time of 0.1 seconds. The only two minor drawbacks of using this shortest exposure time are the following: (i) a non-reproducible large-scale variation in intensity of a very low amplitude (~0.2%) which is due to a slight non-uniformity of the shutter speed, and (ii) a mean count rate which is ~3% lower than those of longer exposures, which is due to an inaccuracy of the shutter timing at this setting. These minor effects occur
only for the shortest exposure times, and disappear completely for exposure times of 0.3 seconds and longer.
All CCD exposures are affected by cosmic rays. The rate of cosmic ray hits in orbit is very high compared to ground-based observations. The current rate at which pixels are affected by cosmic ray hits is 30.0
(± 3.7) pixels per second for the STIS CCD. To allow removal of cosmic rays in post-observation data processing we recommend that whenever possible, given signal-to-noise constraints, you take two or more exposures in any given CCD configuration (see also
Section 11.2.2). The greater the number of independent exposures, the more robust is the removal of cosmic rays and for very long integrations it is convenient to split the exposure into more than two separate images to avoid coincident cosmic ray hits. As an example, for two 1200 sec exposures, about 1250 CCD pixels will be hit in both images and will therefore be unrecoverable. Moreover, since cosmic ray hits typically affect ~5 pixels per event, these pixels will not be independently placed, but rather will frequently be adjacent to other unrecoverable pixels. In general, we recommend that individual exposures should not exceed ~1000 sec duration to avoid excessive amounts of uncorrectable cosmic rays in the images. However, observers must balance the benefit of removing cosmic rays against the loss in signal-to-noise that results from the splitting of exposures when in the read noise-limited regime.
In observations of faint sources, particularly for dispersed light exposures, the intrinsic count rates can be very low. The exposure time needed to reach a break-even between the read-out noise and the Poisson noise per pixel associated with the minimal sky background is ~15 minutes for imaging in
50CCD mode, and ~36 minutes for slitless spectroscopy with G750L. With a dark current of 0.009 e
− sec
−1 it takes 35 minutes of integration for the Poisson statistics on the detector background to equal the read noise. Therefore, repeated short exposures of faint sources can significantly increase the total noise from added readouts. Selecting the correct number and length of repeated integrations requires a consideration of the trade-off between increased read noise and more robust cosmic ray elimination. The
STIS Exposure Time Calculators, or the S/N plots in
Chapter 13 and
Chapter 14, can help you determine whether your observations are in the read noise dominated regime.
Hot pixels, caused by radiation damage, occur in the STIS CCD. Dark frames were routinely obtained twice a day in order to maintain a master list of hot pixels and to update the pipeline superdark reference files on a weekly basis. On a monthly time scale, the CCD was raised to ambient temperature, from its normal operating temperature of ~ –83° C, in order to permit annealing of hot pixels.
Analysis of on-orbit data has shown that the annealing process is successful in that at least ~80% of transient hot pixels (hotter than 0.1 electron sec
−1 pix
−1) are annealed away each month. Apart from the transient hot pixels, there is a substantial number of hot pixels that stay persistently hot after anneals. In 2004, ~1.8% of the pixels of the STIS CCD were persistently hot. The total number of hot (>0.1 electron sec
−1 pix
−1) pixels was ~34,000 after an anneal, as of October 2009 (see
Figure 7.9). The different points in
Figure 7.9 represent pixels with dark current above each listed threshold. Note the increase in hot pixels with time. The break in the trend near day 1600 reflects the switch to the STIS Side-2 electronics. In this figure, side-2 darks were scaled to a housing temperature of 18°C, which corresponds to a detector temperature lower than the
−83°C setpoint that was used when the Side-1 electronics were functional. A detailed description of the variation in hot pixel numbers since launch can be found in
STIS ISR 1998-06.
Note that both binned and spectral data will increasingly suffer from the effects of hot pixels as the percentage of non-annealed pixels increases. Just prior to an anneal, up to 3.5% of all CCD pixels are hot, i.e., both persistent and “annealable” hot pixels. In the case of spectral data, with a normal extraction box height of 7 pixels, this means that 14% of the extracted pixels will be affected by a hot pixel. For imaging data involving rectification, the rectification process interpolates unremoved hot pixels into the four adjacent pixels. For the case of M
×N binning, therefore, 4
×M
×N pixels will be affected by a combination of the binning and rectification process.
While post-pipeline calibration using appropriate STIS reference superdarks allows one to subtract most hot pixels correctly (to within the accuracy set by Poisson statistics), the best way to eliminate all hot pixels is by
dithering (making pixel-scale positional offsets between individual exposures). Dithering as a method of data taking is described in detail in
Chapter 11. An HST handbook on dither strategies and advantages, together with example data is available on-line at:
Analysis of CCD images taken during ground calibration and in Cycle 7 has revealed low-level changes in the bias pattern (at the tenths of a DN level) and a low-level amplifier nonlinearity. This non-linearity (“amplifier ringing”) was uncovered during the analysis of the overscan region on flat field images (reported in
STIS ISR 1997-09). The bias value of a given row in the serial overscan region of flat field images is
depressed with respect to the nominal bias value by an amount proportional to the mean signal in that row. However, the small proportionality factors and low DN levels at which the nonlinearity occurs render the problem negligible for most STIS scientific applications. Instances of data that may be slightly affected by this problem (at the <1% level) are aperture photometry of faint sources (in imaging mode), especially in the case of a crowded region with nearby bright sources that would cause a local depression of the bias value, and photometry of diffuse extended objects that cover a large number of pixels. The brightest hot pixels (see
Section 7.3.5) also cause a measurable local depression in the bias value, but their effect is corrected by using the appropriate superdark reference file (or daily dark file) during CCD calibration.
Observers taking full-frame CCD images obtain both physical overscan (i.e., actual CCD pixels; columns 1-19 and 1016-1062 on the raw image) and virtual overscan (i.e., added electronically to the image; rows 1-20 on the raw image) on their frames; the virtual overscan is not subject to the amplifier nonlinearity problem and can be used to estimate the importance of this effect in the images. Observers using subarrays (e.g., to reduce the time interval between reads and limit the data volume when performing variability observations in the optical; see also
Chapter 11) will obtain only the physical overscan.
Radiation damage at the altitude of the HST orbit causes the charge transfer efficiency (CTE) of the STIS CCD to degrade with time. The effect of imperfect CTE is the loss of signal when charge is transferred through the CCD chip during the readout process. As the nominal read-out amplifier (Amp D) is situated at the top right corner of the STIS CCD, the CTE problem has two possible observational consequences: (1) making objects at lower row numbers (more pixel-to-pixel charge transfers) appear fainter than they would if they were at high row numbers (since this loss is suffered along the
parallel clocking direction, it is referred to as
parallel CTE loss);
and (2) making objects on the left side of the chip appear fainter than on the right side (referred to as
serial CTE loss). In the case of the STIS CCD, the
serial CTE loss has been found to be negligible for practical purposes. Hence we will only address
parallel CTE loss for the STIS CCD in this Handbook.
The current lack of a comprehensive theoretical understanding of CTE effects introduces an uncertainty for STIS photometry. The CTE problems are caused by electron traps in the CCD that are filled as charge passes through the pixels. However, not all traps are accessible to all electrons passing through. Some traps are only accessible if there is significant charge involved. This model suggests that there will not be significant CTE losses in the presence of background, particularly for faint stars, because background electrons fill the traps before the charge associated with such stars passes through. There will still be some loss for brighter stars with background, because their charge may access traps that are unaffected by the background that previously clocked through. Faint stars in areas with little background may suffer from larger losses.
In general, the amount of (parallel) CTE loss depends on the elapsed time on orbit, the distance (i.e., the number of CCD rows) from the source location on the CCD chip to the readout amplifier, the source signal, and the background level.
It should be noted at the outset that the effect of CTE loss has not, as yet, been incorporated into the STIS Exposure Time Calculators (ETCs). Thus, should you believe the CTE losses described herein may impact your spectroscopic or imaging observing program, you will need to provide longer exposure times in your Cycle 18 Phase II proposal to compensate for the anticipated losses1. In particular, Cycle 18 observers using the STIS CCD to observe faint targets (especially in spectroscopic mode) producing less than a few hundred electrons above a low background, are advised to adjust their exposure times appropriately (within the restrictions of their allocated number of HST orbits). CTE effects can be estimated using an iraf script available at:
Analysis of a comprehensive calibration program has allowed us to derive a formula to correct spectroscopic observations of point sources for the parallel-register Charge Transfer Inefficiency (CTI = 1-CTE). This correction has been implemented in the standard calibration pipeline. For spectra at the standard reference position at the CCD center, CTE losses as big as 20% are corrected to within 1% at high signal levels, and to within ~1.5% at low signal levels of ~100 electrons. Further information on CTE loss in spectroscopic mode, including the CTI correction formula, can be found in
STIS ISR 2006-03. The correlation of fractional signal loss and the shift of the centroid of the spectrum is demonstrated in
STIS ISR 2006-01. For the CCD imaging mode, no correction is available at present in the pipeline, and we refer the reader to
Goudfrooij and Kimble’s 2002 HST Calibration Workshop article for the parametrization of the CTE loss and Goudfrooij et al.,
PASP,
118, 1455, 2006.
Figure 7.10 depicts the amount of CTE loss suffered as a function of source signal and background level, for spectra taken at epoch 2011.25 with the target at the center of the detector (solid lines) and at the E1 aperture position (dashed lines). Note that the CTE loss can be significant. A typical spectrum with a signal of about 150 electrons per pixel along the dispersion direction (extracted over the spatial extent of the PSF) and a background level of 5 electrons per pixel (appropriate for a 1000 sec exposure in G430L mode) is expected to experience a CTE loss of ~34% at epoch 2011.25 when located in the center of the CCD, and a loss of ~10% when placed at the E1 aperture position (discussed below), which is much closer to the readout amplifier. For a background of 1 electron per pixel (e.g., a 200 sec exposure), a spectrum with the same source signal level would suffer a CTE loss of ~36% if placed at the center of the detector, and ~11% at the E1 aperture position. This emphasizes the need to take CTE losses into account when estimating exposure times needed to accomplish your science goals.
For the observer, a few strategies for minimizing the effect of CTE loss should be noted. First of all, one should maximize the exposure time whenever possible in order to increase the object counts and the sky background per exposure, both of which reduce CTE loss. Users who are thinking about dithering and shortening their exposure times (e.g., to allow for more dither positions) may want to take this into account. Furthermore, to reduce the number of charge transfers and the consequent loss of signal as illustrated above, observers using the CCD for long-slit spectroscopy of sources having a spatial extent of less than about 3
″ are urged to use the pseudo-apertures located near row 900 of the CCD (the
52X*E1 apertures; see
Section 7.3.8).
Decreasing charge transfer efficiency in the STIS CCD has a detrimental effect on faint spectra acquired at the default location at the center of the chip. For sources with fluxes less than ~1
× 10
-16 erg cm
-2 s
-1 Å
-1, less than ~100 electrons are accumulated per pixel in exposure times of 1000 s or less. (This is the longest integration time we recommend due to the deleterious impact of multiple cosmic rays in a
CR-SPLIT at longer integration times.) At signal levels of 50 - 100 e
-, 25% or more of the charge can be lost during readout due to charge-transfer inefficiencies. Many STIS science programs have fluxes in this range. For spectra of point sources and compact objects such as galactic nuclei, the full length of the slit is not needed. A target location closer to the read-out amplifier near the end of the slit can decrease the charge lost during parallel transfers by a factor of ~4. One could achieve this offset through the use of offset targets or appropriate
POS-TARG entries on the Phase II proposal, but these methods are a bit cumbersome and can be prone to error.
Therefore, for first-order spectra we have defined a set of E1 pseudo-apertures that use the same physical long slits available for STIS CCD observations, but have their default target placement near row 900, ~5 arcseconds from the top of the STIS CCD. This is schematically illustrated in
Figure 7.11. Observers can use these aperture names to place their targets at this location in a rather transparent fashion.
The E1 aperture names and the approximate Y location of the resulting spectra are given in
Table 7.5. Use of the E1 aperture name eliminates the need to specify an offset for the
ACQ/PEAK and a
POS-TARG. These apertures are also recognized by the calibration pipeline software, so spectra are extracted from the correct location using appropriate wavelength solutions, spectral traces, and background regions. For optimum throughput when using these apertures, we recommend using an
ACQ/PEAK exposure to center the target in the aperture when using aperture
52X0.1E1 and
52X0.05E1. While use of these apertures will ameliorate CTE losses, we caution observers to carefully assess the potential impact on their science programs due to the decreased spatial coverage and the relative locations of the bars on the slit.
In the optical, each photon generates a single electron. However, in the near UV, shortward of ~3200 Å there is a finite probability of creating more than one electron per UV photon (see Christensen, O.,
J. App. Phys.
47, 689, 1976). Users will need to take this into account when calculating signal-to-noise ratios and exposure times for the
G230LB and
G230MB gratings, as described in
“Special Case: Spectroscopic CCD Observations at λ < 2500 Å”.
Initial laboratory testing of STIS CCDs showed that excessive illumination by UV light can cause an elevation in residual dark current, due to a surface chemistry effect. However, the actual STIS flight CCD was tested for this effect during ground calibration by the STIS IDT and the effect was found to be much less than previously suspected; this effect is now a concern
only for clear
(50CCD) imaging of
extremely UV-bright targets. Observations of fields with UV-bright objects should be dithered (i.e., positional offsets applied between readouts) to ensure that the UV tail from bright sources does not cause a residual elevation of the dark current for subsequent science observations. It is also recommended to use the longpass-filtered aperture,
F28X50LP, rather than the
50CCD clear aperture, during target acquisitions (see also
Section 8.2.3) when possible. The specific results of the ground testing on the effect of UV overillumination are summarized in
Table 7.6. Note that at launch in 1997 the median STIS CCD dark current was about 0.0015 counts/pixel/second.