9.6 Exposure-Time Examples


In the following you will find a set of examples for the three different channels and for different types of sources. The examples were chosen in order to present typical objects for ACS and also to present interesting cases that may arise with the use of ACS.

Actual ETC calculation results may differ slightly from these published values due to recent improvements in the ETC tables.

9.6.1 Example 1: WFC Imaging a Faint Point Source

What is the exposure time needed to obtain a signal-to-noise of 10 for a point source of spectral type F2V, normalized to V = 26.5, when using the WFC, F555W filter? Assume a GAIN of 1, a box size of 11 × 11 pixel2, and average sky values.

The ETC gives a total exposure time of 4866 seconds to obtain this S/N in a single exposure. Since such an exposure would be riddled with cosmic rays and essentially useless, it is necessary to specify how many exposures to split the observation into. ACS WFC observations generally should be split if the exposure time is larger than about 11 minutes, but for multi-orbit observations, splitting into 2 exposures per orbit is generally sufficient.

For a typical object visibility of 53 minutes, after applying the requisite overheads (see Chapter 8), there is time for two 1200 second exposures per orbit. The required exposure time can thus be reached in 4 exposures, but re-running the ETC using CR-SPLIT = 4 raises the required exposure time to 5339 seconds (because of the extra noise introduced by the four extra readouts). To achieve the required exposure time would require CR-SPLIT = 5, or three orbits.

Using the pencil and paper method, Table 9.1 gives \int QTd\lambda/\lambda = 0.0776, and the ABV correction term can be retrieved from Table 10.1 as 0.02. According to Figure 5.12, a circular aperture of radius 0.3 arcseconds (which has an area of 116 pixels, close to the 121 pixel box specified) encloses about 88% of the light from a star.

The count rate is given by Equation 8 in Section 9.2.1:

C = (2.5\times10^{11}) \times 0.0776 \times 0.88 \times 10^{-0.4(26.5 + 0.02)} = 0.421\ \mathrm{counts/second,}

which agrees with the ETC-returned value of 0.435.

The exposure time can then be found by using Equation 3 in Section 9.3.1, which gives t = 4811 seconds, which is close to the ETC-derived value of 4866 seconds (CR-SPLIT = 1). We have inserted the background rate from Table 9.1 (Bsky =  0.0538) and Table 3.1 (Bdet = 0.0132), and assumed that the noise on the background is much greater than the readout noise.

Note that this can be greatly shortened by specifying a smaller analysis box (for example, 5 × 5) and using LOW-SKY. Dropping the aperture size to 5 × 5, which still encloses 80% of the light, requires 1404 seconds at average sky. Including both the smaller 5 × 5 box and LOW-SKY (Zodiacal = LOW, Earthshine = AVERAGE), using the ETC gives the required exposure time as only 1314 seconds with CR-SPLIT = 1, or 1452 seconds with CR-SPLIT = 2. The LOW-SKY visibility per orbit is 47 minutes, which allows a total on-target exposure time of 2000 seconds in one orbit with CR-SPLIT = 2.

9.6.2 Example 2: SBC Objective Prism Spectrum of a UV Star

What is the peak count rate using the PR110L prism in the SBC for the HST standard star HS2027+0651 (V = 16.9) that was used for the STIS prism calibration? This spectrum is not in the ETC list, therefore we quote below the flux which can be found by dearchiving the STIS spectrum.

The sensitivity peaks in the 1500 Å to 1600 Å region. To find the count rate at 1537 Å, inspection of Figure 6.22 gives the sensitivity of 7.7 × 1014 counts/second/(erg/cm2/s/Å). Multiplying by the stellar flux of 5.3587 × 10–14 gives 41.3 counts/second, summed in the cross dispersion direction. For the fraction of light in the central pixel ε = 0.31, the brightest pixel at 1437.6 Å is 12.9 counts/second/pixel, well below the bright object limit.

The SBC has no readout noise, and the dark current rate is negligible, while the main sky contribution for PR110L is from Lyman-α. For daytime Lyman-α intensity of 20kR = 6.1 × 10–13 ergs/cm2/second/arcseconds2, S =  1.81 × 1014, and d, the dispersion in Å/pixel, is 2.58. Therefore, the background count rate is given by Equation 3 in Section 9.4.2:

B_{\mathrm{sky}}^L = (6.1\times10^{-13}) \times (1.81\times10^{14}) \times 0.032^2/2.58 = 0.044\ \mathrm{counts/sec/pix}.

This value varies somewhat over the field, as the plate scale varies from the nominal 0.032 arcseconds/pixel. For faint source spectroscopy, it is better to use PR130L, which is on a CaF2 substrate to block Ly-α.

9.6.3 Example 3: WFC VIS Polarimetry of the Jet of M87

What signal-to-noise ratio is reached in three one orbit exposures (~2400 seconds each) for M87, when using the WFC, F555W for one orbit each in the three VIS polarizers? Gain is 2, box size is 5 × 5 pixel2CR-SPLIT = 2, and average sky.

If the M87 jet region has μV = 17 magnitudes/arcseconds2, using the ETC with a flat continuum spectral distribution and an exposure time of 2400 seconds (CR-SPLIT = 2), gives S/N = 321 for an observation with each VIS polarizer filter (which is an average of the polarizer at the 3 available position angles 0°, 60°, and 120°). If the polarization P is 20%, then P × S/N = 64.2, so using Equation 6 in Section 6.1.2σP/P  = 0.013, or σP  = 2.6 × 10–3, which is the error on the fractional polarization. The error on the position angle, σθ, is 0.4° using Equation 7 in Section 6.1.2.

9.6.4 Example 4: SBC imaging of Jupiter's Aurora at Lyman-alpha

What signal-to-noise ratio is reached in a one orbit exposure (2000 seconds) observing Jupiter's aurora in Ly-α using the SBC and F122M filter?

Equation 10 in Section 9.2.1 can be used to calculate the expected count rate. The aurora is variable, up to ~100kR. The value of (QT) for the SBC+F122M filter at 1216 Å is 0.0126, from inspection of Figure 10.104 and checking the throughput of the bandpass with pysynphot. For a surface brightness of 40kR = 1.22 10–12 erg/cm2/second/arcseconds2 (see Section 9.4.2 for conversion), the total counts per pixel are

Ct = (2.23\times10^{12}) \times 0.0126 \times (1.22 \times 10^{-12}) \times 1216 \times 0.032^2 \times 2000 = 85.56\ \mathrm{counts/pix}.

The background contributions are the detector dark of 8.11 10–6 counts/pixel/second (which can be ignored in this case) and a sky background which is dominated by geocoronal Lyman-αUsing the same formula listed in Example 9.6.2, Equation 3 in Section 9.4.2, we compute the geocoronal background from Lyman-α in the F122M bandpass. During the daytime, the geocoronal background count rate is 0.022 counts/second/pix, while at night the value drops to one tenth of this, or 0.0022 counts/second/pix. After 2000 seconds of integration, the Lyman-α background is 43.7 counts/pix and 4.37 counts/pix for day and night, respectively. 

Finally, we calculate the signal-to-noise ratio Σ for a 2 × 2 pixel2 resolution element. In the daytime,

\Sigma = \frac{CtN_{\mathrm{pix}}}{\sqrt{(Ct + Bt)N_{\mathrm{pix}}}} = \frac{85.56 \times 4}{\sqrt{(85.56 + 43.7)\times 4}} = 15.05,

and at night,

\Sigma = \frac{88.1 \times 4}{\sqrt{(88.1 + 4.37)\times 4}} = 18.04.

9.6.5 Example 5: Coronagraphic imaging of the Beta-Pictoris Disk

In this example, using the now inoperative HRC, we shall consider the case where we are trying to determine the S/N achieved on the Beta Pictoris disk, assuming a disk surface brightness of 16 magnitudes/arcseconds2 in the R band at a distance of 6 arcseconds from the central star with a V magnitude of 3.9, for an exposure time of 1000 seconds with an F435W filter. Assume that the star and disk have an A5V-type spectrum. Using the ETC and considering the case for the 3.0 arcseconds occulting mask:

  • Disk count rate = 4.98 e/second for a 2 × 2 pixel2 aperture (including 47.5% throughput of coronagraph).
  • Sky count rate = 0.010 e/second/pixel.
  • Detector dark rate = 0.012 e/second/pixel.
  • In 1000 seconds, this gives 4,980 e/(2 × 2 pixel2) aperture in the disk region.
  • Central star count rate = 3.63 × 108 e/second in a 101 × 101 pixel2 aperture (101 × 101 pixel2 aperture used to estimate total integrated flux).
  • At a distance 6 arcseconds from the central star, the fraction of flux per square arcsecond in the PSF wings is 2.6 × 10–6.  BPSF = (3.63 × 108) × (2.6 × 10–6) = 943.8 e per square arcsecond. The counts collected in 4 pixels are 4 × 0.0272 × 943.8  = 2.752.
  • The S/N in a 2 × 2 pixel2 box is then \Sigma = \frac{4980}{\sqrt{4980 + 2.8}} = 70.5.

9.6.6 Example 6: WFC Imaging: Post-Flash to Mitigate Low Sky

WFC images with low background (below ~30 e/pixel of sky plus dark current) suffer increasingly severe CTE losses far from the serial registers. In some cases, it may be advantageous to post-flash such images to improve recovered signal-to-noise. In the following ETC example, we incorporate post-flash to boost the background for a single 90-second exposure with filter F850LP and "average" levels for earthshine, zodiacal light, and airglow.

We configure the ETC to calculate the S/N ratio obtained in 90 seconds with WFC using the F850LP filter (with CR-SPLIT = 1). The ETC also reports the background level as usual. For this example, the flux of the target is irrelevant. Adopting a photometry region of 1 × 1 pixel2 for simplicity, and otherwise using default settings, the ETC results page includes a low-background warning (currently triggered below 20e per pixel of sky plus dark current) near the top of the report. In this example, the expected background level is only 4.37e/pixel (3.55e from the sky and 0.83e from dark current).

Depending on science goals, supplementing this background with post-flash may be a viable solution. For the current example, adding a post-flash of 25e on the ETC front page results in the low-background warning no longer triggering, as well as a reduction of the reported S/N because of the increased background. However this extra post-flash would considerably boost the recovered signal for sources far from the serial register, resulting in a net gain in S/N for such sources. The ETC is not currently capable of estimating WFC CTE-induced signal losses. The ACS Team has provided such a calculator, suitable for point-source photometry, at the ACS CTE Calculator website.

The above example should be treated with caution, however, for the following reasons:

  • There is nothing ideal about a WFC background of 25–30 e/pixel. In general, a higher background reduces CTE losses at the cost of added noise, and the optimal post-flash level will depend upon source position and intensity.
  • The lowest ETC settings for earthshine, airglow, and zodiacal light may occasionally overestimate actual WFC background levels, based upon recent comparisons with Cycle 18 observations (ACS ISR 2012-04). Users especially concerned with CTE should err on the side of lower-than-predicted background when determining how much post-flash to add.
  • As shown in Figure 9.4, the WFC post-flash illumination declines by 50% with radius from the detector center, with approximately azimuthal symmetry. When the post-flash is the dominant source of background, both the noise properties and the degree of CTE mitigation across the image will therefore be highly nonuniform. The non-uniformity is such that the post-flash signal is highest where CTE losses have the most effect, i.e., far from the amplifier in the parallel transfer direction. As a consequence, mitigation of CTE losses will be best for the sources that need it the most. However, the nonuniform noise of the post-flash background will require a careful treatment during subsequent analyses.
  • For users desiring to use the post-flash capabilities, it is recommended to read Section 5 of ACS ISR 2018-02. The APT assumes a single value of 14 e-/sec to compute the flash duration required to achieve a specified signal (e.g., for a 20e- post-flash, t = 20e-/(14 e-/sec) = 1.4 seconds). Due to the nonuniform post-flash signal, this flash rate could be an overestimation of the true post-flash signal. The aforementioned ISR provides a convenient method for computing the necessary scaling factor to ensure the desired number of electrons are deposited at the location of your source.

ACS ISR 2018-02 and ACS ISR 2014-01 provide detailed guidance for the appropriate use cases of post-flash.

Figure 9.4: Post-flash reference file for ACS/WFC

The creation of a post-flash reference image free of dark current artifacts is described in ACS ISR 2018-02. Contours at 10, 12, and 14 e-/sec highlight the non-uniformity of the LED illumination pattern.