operating modes for the CCD and MAMAs, which produce a time- integrated accumulated image. These are the most commonly used modes.
operating mode for the MAMA detectors, which outputs an event stream of high-time-resolution observations in the ultraviolet (UV).
(acquisition) and ACQ/PEAKUP
operating modes for the CCD and MAMAs used to acquire targets in the spectroscopic slits and behind coronagraphic bars and masks. Target acquisitions are described in Chapter 8
The STIS CCD has only the single operating mode, ACCUM
, for science data. The CCD pixels accumulate charge during the exposure in response to photons. The charge is read out at the end of the exposure at a selectable gain (number of e-/DN) and converted to 16 bit data numbers (DN) by the A-to-D converter. The DN are stored as 16 bit words (with a range 0 to 65,535) in the STIS data buffer memory array. At the default CCDGAIN=1
, the gain amplifier saturation level (33,000 electrons), and not the 16-bit format, limits the total counts that can be sustained in a single exposure without saturating (see also Section 7.2.10
and Section 7.3.2
). At the other supported gain, CCDGAIN=4
, the CCD
full well (which can be as low as 120,000 e- or 30000 DN in some regions of the detector) still determines the saturation limit.
A full detector readout is actually 1062 ×
1044 pixels with physical and virtual overscans. Scientific data are obtained on 1024 ×
1024 pixels, each projecting to ~0.05 ×
0.05 arcsecond on the sky. The dispersion axis runs along AXIS1
(image X or along a row of the CCD), and the spatial dimension of the slit runs along AXIS2
(image Y or along a column of the CCD). Figure 11.1
illustrates the full CCD format and its orientation with respect to the spacecraft (U2 and U3 or V2 and V3) axes. Arrows indicate the orientation of the parallel and serial clocking. The readout directions depend on the amplifier used. For the default amplifier D, the readout is at the upper right corner. It includes 19 columns of leading and 19 columns of trailing physical overscan in AXIS1
, and 20 trailing rows of virtual overscan in AXIS2
. The trailing serial overscan as well as the parallel overscan pixels are used to determine the bias level in post-observation data processing. The parallel overscan can also be used in the diagnosis of charge-transfer problems.
The minimum CCD
exposure time is 0.1 second and the maximum possible exposure time is 4.7 hours (though we cannot imagine wanting a single exposure longer than 60 minutes). The minimum time between identical
exposures for CCD
full-frame (1062 ×
1044) images is ~45 seconds.1
This time is dominated by the time it takes to read out the CCD (29 seconds for the full frame) and can be reduced to ~19 seconds if you use a subarray (see “CCD Subarrays”
The CCD supports on-chip binning. When on-chip binning is used the specified number of pixels in the serial and parallel directions are read out as a single pixel. The advantage of CCD binning is that the read noise per binned pixel is comparable to the read noise per unbinned pixel. Thus if your signal-to-noise per pixel is dominated by read noise when no binning is used, you can increase the signal-to-noise by binning. The dis
advantages of using on-chip binning are (a) it reduces the resolution of your spectrogram or image, (b) the relative number of pixels affected by cosmic rays increases, and (c) the relative number of ‘hot’ pixels (which is ~5% of all CCD pixels for unbinned data by the time this handbook is issued, see Chapter 7
), increases by a factor proportional to the binning factor. On-chip binning of 1, 2, or 4 pixels in both the AXIS1
directions is supported. Note that on-chip binning is not allowed when subarrays are used.
The number of hot pixels has been increasing steadily with time due to accumulated radiation damage on the STIS CCD (see the discussion on hot pixels in Chapter 7
). Thus the impact of hot pixels on binned data has become significantly larger. Also note that when spectral data are spatially rectified, a single pixel in the original data will be interpolated into four pixels in the rectified image. For data binned N ×
M on board the spacecraft, a single bad pixel will, after rectification, affect the equivalent of 4 ×
M pixels in an unbinned image.
When using the ETC
to estimate the effects of on-board binning on the S/N of CCD observations, be aware that increasing the binning in the dispersion direction may cause the ETC
to use a larger resolution element for its S/N calculation. Be sure to understand how much of any increase in the S/N number output by the ETC
is due to an actual decrease in the read noise and how much is simply due to a change in the size of the resolution element assumed for the calculation.
As described in Section 11.1.1
, full-frame CCD readouts are composed of 1062 ×
1044 pixels: 1024 ×
1024 data pixels, 19 leading and 19 trailing serial overscan pixels, and 20 trailing parallel overscan pixels. Dispersion runs along axis1
and the long dimension of the slit runs along axis2
. Subarrays are required to span the full width of the CCD detector in the serial (dispersion) direction in order to ensure they contain the serial overscan needed to determine the bias level; however, you can control the height of the subarray in the parallel direction (i.e., along the slit for long-slit spectroscopic observations). Note that no parallel overscan is returned for subarrays (see Section 7.3.6
). Subarray size is specified in Phase II by the parameter SIZEAXIS2
, the size in pixels of the subarray in the AXIS2
The minimum allowed value of SIZEAXIS2
for ACCUM mode observations is 30 pixels (corresponding to 1.5 arcseconds), and SIZEAXIS2
must be an even number of pixels. By default the target is placed within a few pixels of the center of the subarray. For a few central wavelength settings, however, the target may be systematically offset by up to 30 pixels in the spatial direction. Observers should consult with the Help Desk
prior to using SIZEAXIS2
with a value of less than 64 pixels.
The format of the data you receive when you use a CCD subarray will have dimensions 1062 × SIZEAXIS2
, will cover the full range in the dispersion direction, and will include the serial overscan. The STIS buffer can hold seven full-frame CCD exposures at one time, or 7 ×
(1024 / SIZEAXIS2
) exposures at any one time. Full-frame CCD data acquired in one exposure can be transferred to the HST data recorder during the subsequent exposure(s) so long as the integration time of the subsequent exposure is longer than 3.0 minutes. If you are taking a series of exposures which are shorter than that, the buffer cannot be emptied during exposure, and once the STIS buffer fills up, there will be a pause in the exposure sequence of roughly 3 minutes as the buffer is emptied. This problem can sometimes be avoided with the judicious use of subarrays.
In MAMA ACCUM
mode exposures, photons are accumulated into a 2048 ×
2048, 16-bit-per-element oversampled array in the STIS data buffer memory as they are received. At the end of the exposure, the data can be left in the over-sampled (or highres) format, which is the default for scientific exposures, or they can be binned along AXIS1
to produce a 1024 ×
1024 native-format image. ACCUM
is the mode of choice for all observations that do not require time resolution on minute or less scales. Dispersion runs along AXIS1
and the spatial dimension of the slit runs along AXIS2. Figure 11.3
and Figure 11.4
illustrate the format and coordinate system for MAMA images, showing how first-order and echelle ACCUM
mode spectrograms appear. PRISM
images have dispersion along AXIS1
. Note that for FUV-MAMA G140L
the target is placed near AXIS2=392
to ensure that it will not fall on the shadow of the repeller wire (see Section 7.6
). Thus there will be ~3 arcseconds less spatial sky coverage to decreasing AXIS2
and ~3 arcseconds more spatial sky coverage to increasing AXIS2
along the slit. Said another way, slit center will project ~3 arcseconds below the detector center along AXIS2
observations. Data taken prior to March 15, 1999 have the slit center offset above
the detector center. Note also the effects of the monthly offsetting which applies to all MAMA modes (see Section 7.6
The minimum MAMA ACCUM
mode exposure time is 0.1 second and the maximum exposure time is 1.8 hours. The minimum time between identical
exposures is ~30 seconds, for exposures which are longer than 3 minutes, and it is 2.5 minutes for exposures which are shorter than 3 minutes. This difference arises because in the former case the buffer can be dumped to the HST recorder during the subsequent exposure (i.e., in parallel), but in the latter case there is insufficient time to dump the buffer during the subsequent exposure and the buffer must be dumped serially (i.e, using observing time).
For the MAMA medium-resolution first-order modes and medium and high-resolution echelle modes (i.e., gratings G140M
, and E140H
), a correction for Doppler shifting of the photon energies due to HST spacecraft motion is applied as the photons are counted, prior to their addressing in STIS data buffer memory. The leading and trailing pixels in the dispersion direction (AXIS1
) for Doppler-corrected exposures therefore receive less effective integration time, since source photons at the corresponding wavelengths have been Doppler-shifted off the edge of the detector for some fraction of the total exposure time. This effect is strongest in the high-resolution echelle modes, where for a maximum HST spacecraft velocity of 7.5 km/s, the leading and trailing ~20 AXIS1
pixels will have reduced effective exposure times.
The MAMA detectors record scientific data in the so-called highres
mode, producing 2048 ×
2048 images of super resolution - one half the 1024 ×
1024 native format
pixel size defined by the anode readout itself. All scientific data are taken in this format by default. Below we explain in more detail the nature of highres data.
The MAMA detectors have 1024 ×
1024 physical or so-called native-format pixels. However, each count is detected by multiple electrodes, so the charge distribution among the electrodes can be used to centroid the incident charge cloud to subpixel resolution. The gain of the highres 2048 ×
2048 mode is a ~10–30% increase in resolution at the price of the increased fixed-pattern noise due to poorly characterized charge partition among the electrodes. The highres flat fields have much more structure than the 1024 ×
1024 flats, with adjacent columns and rows differing by ~30% in an off/on pattern whose variability is appreciably higher than for 1024 ×
1024 format images. This effect and the inherently lower signal-to-noise ratio in the full resolution flat-field images (nominally ~20 to 1 per highres pixel) suggest that it may be difficult to routinely realize the benefit in resolution. However, we note that data taken in highres mode can always be binned to 1024 ×
1024 on the ground in post-observation data processing, and since the extra overheads in highres mode are typically quite small, highres is the default data-taking mode for the MAMA. The pipeline bins the data to 1024 ×
1024 format during calibration so that the pipeline output calibrated images are native format (see the STIS Data Handbook
for more details).
mode is used for high-time-resolution spectroscopy and imaging in the UV. When used in TIME-TAG
mode, the MAMA produces an event stream of AXIS1
, and TIME
data points, with a time resolution of 125 microseconds. The volume of data produced in TIME-TAG
mode can be very large and the data therefore must be continuously transferred from the STIS internal buffer to the data recorders to sustain TIME-TAG
exposures of any significant duration.
The axis orientation in TIME-TAG i
s the same as in ACCUM
mode (see Figure 11.3
). The spacecraft time (absolute zero point of the time) is routinely known to 10 millisecond accuracy. No Doppler correction is applied by the flight software for TIME-TAG
mode, but the correction can be applied during the post-processing of the data. The recorded times are the spacecraft times, which can be converted to heliocentric times using the ephemeris of the Earth and the spacecraft. TIME-TAG
mode is illustrated in Figure 11.5
. Processing of TIME-TAG
data by the STScI pipeline is described in Section 15.1
mode, events detected on the anode wires are queued in a 4096-event first-in first-out (FIFO) prior to time assignment and subsequent storage in a STIS memory buffer. When the FIFO is less than half full, 4 events can be processed during each 125 microsecond tick of the STIS clock, corresponding to a maximum stable count rate of 32,000 counts/s. Times are assigned shortly after detection, when the event is extracted from the FIFO. This is the desired operating state in TIME-TAG
mode. Higher count rate situations (described below) should be avoided because they result in less accurate times, lost events, and buffer management problems.
observations, STIS memory is divided into two 8 megabyte buffers, each of which can hold up to 2 ×
events. If the cadence between scheduled buffer dumps is at least 99 seconds, then one buffer can be actively recording new events, while previously recorded events in the other buffer are being dumped to an HST data recorder. Thus, events can be dumped to STIS memory without gaps only if the global count rate is below 20,000 counts/s.
|To prevent loss of data, BUFFER-TIME
should be short enough that fewer than 2 ×
events are expected in the interval between dumps. If R is the expected count rate (predicted by the STIS ETC
, for example), then BUFFER-TIME
should be smaller than 2 ×
/R. A bit of margin protects against source variability or inaccurate count rate predictions. Be sure to include sky and detector backgrounds when estimating count rates.
should be at least 99 seconds when more than 2 dumps are expected. Otherwise, the observing sequence will be interrupted whenever both buffers are in the process of being dumped. In such cases it is probably better to choose a BUFFER-TIME
of 99 seconds. This guarantees that photons will be recorded whenever the active buffer has remaining space. If the active buffer fills in less than the selected BUFFER-TIME
, additional photons will be discarded until the next dump begins. Reliable flux calibration is not possible in such cases.
In summary, BUFFER-TIME
should be less than 2 ×
/R, but longer than 1/30 the total exposure time and longer than 99 seconds. As an added precaution against data loss, it is recommended to use a BUFFER-TIME of 1.6 x 106
/R, which adds a 20% safety margin. In some cases it will not be possible to satisfy all of these criteria, in which case multiple short ACCUM
exposures should be considered as an alternative. Figure 11.6
illustrates the process of estimating BUFFER-TIME
refers to the total integration time (in seconds) of all the exposures in the visit, and Texp
refers to the integration time (in seconds) of the particular exposure under consideration.