STScI

Advanced Camera for Surveys Instrument Handbook for Cycle 14

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Chapter 6:
Exposure-Time Calculations


6.1 Overview
    6.1.1 The ACS Exposure Time Calculator
6.2 Determining Count Rates from Sensitivities
    6.2.1 Imaging
    6.2.2 Spectroscopy
6.3 Computing Exposure Times
    6.3.1 Calculating Exposure Times for a Given Signal-to-Noise
    6.3.2 Exposure Time Estimates for Red Targets in F850LP
    6.3.3 Two-Gyro Guiding
6.4 Detector and Sky Backgrounds
    6.4.1 Detector Backgrounds
    6.4.2 Sky Background
6.5 Extinction Correction
6.6 Exposure-Time Examples
    6.6.1 Example 1: WFC Imaging a Faint Point Source
    6.6.2 Example 2: SBC Objective Prism Spectrum of a UV Spectrophotometric Standard Star
    6.6.3 Example 3: WFC VIS Polarimetry of the Jet of M87
    6.6.4 Example 4: SBC imaging of Jupiter's Aurora at Lyman-alpha
    6.6.5 Example 5: Chronographic imaging of the Beta-Pictoris Disk
6.7 Tabular Sky Backgrounds

6.1 Overview


In this chapter, we explain how to use sensitivities and throughputs to determine the expected count rate from your source and how to calculate exposure times to achieve a given signal-to-noise ratio for your ACS observations taking various background contributions into account. At the end of this chapter in "Exposure-Time Examples", you will find examples to guide you through specific cases.

6.1.1 The ACS Exposure Time Calculator

The ACS Exposure-Time Calculator (ETC) is available to help with proposal preparation at:

 http://www.stsci.edu/hst/acs/software/etcs/ETC_page.html. 

This ETC calculates count rates for given source and background parameters, and signal-to-noise ratios for a given exposure time, or count rates and exposure time for a given signal-to-noise ratio for imaging, spectroscopic and coronagraphic observations. A variety of apertures are now available, both circular and square, allowing the user to either select a radius in arcseconds or a size in pixels. The current default are a 0.2 arcsec radius for both the WFC and the HRC and a 0.5 arcsec radius for SBC observations, which enclose approximately 80% of the PSF flux. Square and circular apertures are available between 0.1 and 2.0 arcsec. For extended sources the S/N calculation is based on counts summed over one resolution element of 2x2 pixels, as the source size is assumed to be larger than the ACS resolution. A calibrated spectrum of your source can be provided directly to the Exposure-Time Calculator. The ETC also determines peak per-pixel count rates and total count rates to aid in feasibility assessment. Warnings appear if the source exceeds the local or global brightness limits for SBC observations (see Section 7.5). The ETC has online help for its execution and interpretation of results. Alternatively, users can use synphot to calculate count rates and the wavelength distribution of detected counts.

6.2 Determining Count Rates from Sensitivities


In this Chapter, specific formulae appropriate for imaging and spectroscopic modes are provided to calculate the expected count rates and the signal-to-noise ratio from the flux distribution of a source. The formulae are given in terms of sensitivities, but we also provide transformation equations between the throughput (QT) and sensitivity (S) for imaging and spectroscopic modes.

Throughputs are presented in graphical form as a function of wavelength for the prisms and for the imaging modes in Chapter 10. Given your source characteristics and the sensitivity of the ACS configuration, calculating the expected count rate over a given number of pixels is straightforward, since the ACS PSF is well characterized. The additional required information is the encircled energy fraction (f) in the peak pixel, the plate scale, and the dispersions of the grisms and prisms. This information is summarized in Tables 6.1 to 6.3.


Table 6.1: Useful Quantities for the ACS WFC
Filter
Pivot (Å)
QT d/
AB mag
zero point
S d
encircled
energy
Flux in
central
pixel
Background
sky rate
F435W 4317.4 0.0744 25.67 3.18E18 0.85 0.22 0.0284
F475W 4744.3 0.1070 26.07 5.53E18 0.86 0.21 0.0609
F502N 5023.0 0.0032 22.27 1.88E17 0.86 0.21 0.0020
F550M 5581.2 0.0362 24.89 2.59E18 0.85 0.22 0.0280
F555W 5359.6 0.0775 25.72 5.11E18 0.86 0.21 0.0545
F606W 5917.7 0.1573 26.49 1.26E19 0.85 0.22 0.1358
F625W 6310.5 0.0915 25.90 8.37E18 0.85 0.22 0.0825
F658N 6583.9 0.0050 22.75 5.00E17 0.85 0.22 0.0045
F660N 6599.4 0.0019 21.67 1.87E17 0.85 0.22 0.0017
F775W 7693.0 0.0731 25.65 9.93E18 0.85 0.20 0.0780
F814W 8059.8 0.0948 25.94 1.41E19 0.83 0.19 0.1044
F850LP 9054.8 0.0352 24.86 6.63E18 0.73 0.14 0.0415
F892N 8914.9 0.0036 22.37 6.48E17 0.77 0.15 0.0039
G800L 7480.7 0.1591 26.50 2.04E19 0.86 0.17 0.1526
CLEAR 6269.8 0.3833 27.45 3.46E19 ---- 0.10 0.3580


Table 6.2: Useful Quantities for the ACS HRC
Filter
Pivot (Å)
QT d/
AB mag
zero point
S d
encircled
energy
Flux in
central
pixel
Background
sky rate
F220W 2255.3 0.0106 23.55 1.23E17 0.79 0.17 0.0001
F250W 2715.8 0.0123 23.72 2.09E17 0.82 0.16 0.0003
F330W 3362.7 0.0172 24.08 4.47E17 0.84 0.16 0.0006
F344N 3433.7 0.0017 21.59 4.67E16 0.84 0.16 0.0001
F435W 4311.0 0.0436 25.09 1.86E18 0.86 0.17 0.0043
F475W 4775.7 0.0650 25.53 3.40E18 0.85 0.17 0.0120
F502N 5022.9 0.0021 21.82 1.24E17 0.85 0.17 0.0003
F550M 5579.8 0.0234 24.42 1.67E18 0.85 0.15 0.0048
F555W 5356.0 0.0503 25.25 3.31E18 0.85 0.16 0.0099
F606W 5888.0 0.0983 25.98 7.82E18 0.85 0.14 0.0238
F625W 6295.5 0.0557 25.36 5.07E18 0.84 0.13 0.0148
F658N 6583.7 0.0030 22.18 2.98E17 0.83 0.13 0.0008
F660N 6599.1 0.0011 21.11 1.11E17 0.83 0.13 0.0003
F775W 7665.1 0.0380 24.94 5.13E18 0.78 0.11 0.0111
F814W 8115.3 0.0521 25.29 7.88E18 0.76 0.10 0.0161
F850LP 9145.2 0.0228 24.39 4.37E18 0.68 0.08 0.0075
F892N 8916.1 0.0022 21.87 4.09E17 0.73 0.09 0.0007
G800L 7506.4 0.0924 25.91 1.20E19 0.81 0.07 0.0250
PR200L 5650.2 0.2756 27.10 2.02E19 0.80 0.16 0.0624
CLEAR 5472.0 0.3205 27.26 2.20E19 ---- 0.12 0.0683


Table 6.3: Useful Quantities for the ACS SBC
Filter
Pivot (Å)
QT d/
AB mag
zero point
S d
encircled
energy
Flux in
central
pixel
Background
sky rate
F115LP 1406.1 0.0147 23.92 6.70E16 0.83 0.11 0.0238
F122M 1273.8 0.0010 20.95 3.56E15 0.82 0.09 0.0042
F125LP 1437.5 0.0122 23.71 5.80E16 0.83 0.12 0.0027
F140LP 1527.0 0.0069 23.09 3.68E16 0.84 0.13 0.0000
F150LP 1610.7 0.0038 22.45 2.27E16 0.84 0.14 0.0000
F165LP 1757.9 0.0010 21.02 7.29E15 0.85 0.16 0.0000
PR110L 1429.4 0.0120 23.69 5.62E16 0.86 0.26 0.0129
PR130L 1438.8 0.0120 23.68 5.66E16 0.87 0.28 0.0027

In each Table, the following quantities are listed:

Here, we describe how to determine two quantities:

  1. The counts sec-1 (C) from your source over some selected area of Npix pixels, where a signal of an electron on a CCD is equivalent to one count.
  2. The peak counts sec-1 pixel-1 (Pcr) from your source, which is useful for avoiding saturated CCD exposures and for assuring that SBC observations do not exceed the bright-object limits.

We consider the cases of point sources and diffuse sources separately in each of the imaging and spectroscopy sections following.

6.2.1 Imaging

Point Source

For a point source, the count rate, C, can be expressed as the integral over the bandpass of the filter:

Where:

The peak counts sec-1 pixel-1 from the point source, is given by:

Where:

Again, the integral is over the bandpass.

If the flux from your source can be approximated by a flat continuum (F = constant) and f is roughly constant over the bandpass, then:

We can now define an equivalent bandpass of the filter (B) such that:

Where:

The count rate from the source can now be written as:

In Tables 6.1-6.3, we give the value of for each of the filters.

Alternatively, we can write the equation in terms of V magnitudes:

where V is the visual magnitude of the source, the quantity under the integral sign is the mean sensitivity of the detector+filter combination and is tabulated in Tables 6.1-6.3, and n is the filter-dependent correction for the deviation of the source spectrum from a constant F spectrum. This latter quantity is tabulated for several different astronomical spectra in Tables 10.1 to 10.3 in Chapter 10.

Diffuse Source

For a diffuse source, the count rate, C, per pixel, due to the astronomical source can be expressed as

:

Where:

Emission Line Source

For a source where the flux is dominated by a single emission line, the count rate can be calculated from the equation

where C is the observed count rate in counts/sec, (QT) is the system throughput at the wavelength of the emission line, F() is the emission line flux in units of erg cm-2 s-1, and is the wavelength of the emission line in Angstroms. (QT) can be determined by inspection of the plots in Chapter 10. See Section 6.6.4 for an example of emission-line imaging using ACS.

6.2.2 Spectroscopy

Point Source

For a point source spectrum with a continuum flux distribution, the count rate, C, is per pixel in the dispersion direction and is integrated over a fixed extraction height in the spatial direction perpendicular to the dispersion:

Where:

For an unresolved emission line at with a flux of in
erg sec-1 cm-2 the total counts recorded over the Nspix extraction height is:

These counts will be distributed over pixels in the wavelength direction according to the instrumental line spread function.

In contrast to the case of imaging sensitivity , the spectroscopic point source sensitivity calibration () for a default extraction height of Nspix is measured directly from observations of stellar flux standards after insertion of ACS into HST. Therefore, the accuracy in laboratory determinations of for the ACS prisms and grisms is NOT crucial to the final accuracy of their sensitivity calibrations.

The peak counts sec-1 pixel-1 from the point source, is given by:

Where:

6.3 Computing Exposure Times


To derive the exposure time to achieve a given signal-to-noise ratio, or to derive the signal-to-noise ratio in a given exposure time, there are four principal ingredients:

6.3.1 Calculating Exposure Times for a Given Signal-to-Noise

The signal-to-noise ratio, is given by

:

Where:

This equation assumes the optimistic (and often realistic) condition that the background zero point level under the object is sufficiently well known (and subtracted) to not significantly contribute; in crowded fields this may not be true.

Observers using the CCD normally take sufficiently long integrations that the CCD read noise is not important. This condition is met when:

For the CCD in the regime where read noise is not important and for all SBC observations, the integration time to reach a signal-to-noise ratio , is given by

:

If your source count rate is much brighter than the sky plus detector backgrounds, then this expression reduces further to:

i.e. the usual result for Poisson statistics of .

More generally, the required integration time to reach a signal to noise ratio is given by:

6.3.2 Exposure Time Estimates for Red Targets in F850LP

At wavelengths greater than 7500Å (HRC) and about 9000Å (WFC) ACS CCD observations are affected by a red halo due to light scattered off the CCD substrate. An increasing fraction of the light as a function of wavelength is scattered from the center of the PSF into the wings. This problem affects particularly the very broad z-band F850LP filter, for which the encircled energy depends on the underlying spectral energy distribution the most. In the currently available ETC, the treatment of such an effect has been ameliorated but not solved. The encircled energy fraction is calculated at the effective wavelength which takes into account the source spectral distribution. This fraction is then multiplied by the source counts. (The effective wavelength is the weighted average of the system throughput AND source flux distribution integrated over wavelength). However, this does not account for the variation in enclosed energy with wavelength.

As a consequence, in order to obtain correct estimated count rates for red targets, observers are advised to use the Synphot package in IRAF/STSDAS for which the proper integration of encircled energy over wavelength has now been incorporated. To quantify this new Synphot capability, we compare ETC results with Synphot for a set of different spectral energy distributions and the observation mode WFC/F850LP. In Table 6.4, the spectral type is listed in the first column. The fraction of light with respect to the total integrated to infinity is listed in the other two columns, for the ETC and Synphot calculations respectively. These values are derived for a 0.2 arcsec aperture for the ETC calculations and Synphot.


Table 6.4: Encircled Energy Comparison for WFC/F850LP
Sp. Type
APT ETC
Synphot
O
0.76
0.74
M
0.71
0.7
L
0.69
0.68
T
0.61
0.6

The ETC results are off by 3% (O star), 2% (M star), 2% (L star), and 1% (T star). If this small effect is relevant to particular observations, then the Synphot software package can be used. To learn how to use the synphot tool, we refer to the instructions provided in the April 2003 STAN, http://www.stsci.edu/hst/acs/documents/newsletters/stan0302.html, and in ACS ISR 2003-08.

6.3.3 Two-Gyro Guiding

At some future date HST may be operated with only two gyroscopes, hence causing additional spacecraft jitter and degradation of the effective PSF. This could potentially degrade the signal-to-noise ratio for point sources.

See the Two-Gyro Handbook for detailed information.

We anticipate that a two-gyro version of the ACS Exposure Time Calculator will be available to help assess these impacts.

6.4 Detector and Sky Backgrounds


When calculating expected signal-to-noise ratios or exposure times, the background from the sky and the background from the detector must be taken into account.

6.4.1 Detector Backgrounds

Table 6.5 shows the read-noise and dark-current characteristics of the detectors. See Table 7.3 for further details including variations by amplifier and GAIN for the CCDs.


Table 6.5: Detector Backgrounds
 
WFC
HRC
SBC
Read noise (electrons pix-1)
~5
~4.7
0
Dark current (electrons sec-1 pix-1)
3.2x10-3
3.6×10-3
1.2×10-5

6.4.2 Sky Background

The sources of sky background which will affect ACS observations include:

The background in counts sec-1 pixel-1 for imaging observations can be computed as:

Where:

The image of the sky through a disperser is not uniform, since some wavelengths fall off the detector for regions of sky near the edge of the field of view (FOV). Since the ACS grism spectra are of order 200 pixels long, the regions of lower sky will be strips at the long and short wavelength edges of the FOV. The maximum width of the strips from where the signal starts to decline to the edge, where the signal is down by roughly 2x, is about half the total length of a spectrum of a point source, i.e. roughly 100 pixels in the case of a sky background with a continuum of wavelengths. In the case of the HRC, the sky for the dispersed mode will not have the low background strips, since the FOV is not masked to the detector size. These small strips of lower sky background in the SBC and the WFC are ignored in the following formulae. Furthermore in the SBC and the WFC, since the spectra do not lie along the direction of the anamorphic distortion, the plate scales of and above must be replaced by the plate scales and in the orthogonal spatial and dispersion directions, respectively. Interior to the strips, a point on the detector sees a region of sky over the full wavelength coverage of the disperser. Thus, for spectroscopic observations:

For a monochromatic sky emission line at like Lyman-, which will dominate the background through the LiF prism:

where

The total sky background is:

Figure 6.1 and Table 6.8 show "high" sky background intensity as a function of wavelength, identifying the separate components which contribute to the background. The "shadow" and "average" values of the Earthshine contribution in the ACS Exposure Time Calculator correspond, respectively, to 0 and 50% of the "high" values in Figure 6.1 and Table 6.8. For the zodiacal sky background, the values in Figure 6.1 and Table 6.8 correspond to the high value of mV = 22.1 from Table 6.6, while the "low" and "average" zodiacal light is scaled to mV = 23.3 and 22.7, respectively.

Figure 6.1: High Sky Background Intensity as a Function of Wavelength. The zodiacal contribution (ZL) is at ecliptic latitude and longitude of 30,180 degrees, and corresponds to mv = 22.7 per square arcsec. The Earthshine (ES) is for a target which is 24 degrees from the limb of the sunlit Earth. Use Figure 6.2 to estimate background contributions at other angles. The daytime geo-coronal line intensities are in erg cm-2 s-1 arcsec-2 (see Table 6.7).


 

Background Variations and LOW-SKY

In the ultraviolet, the background contains bright airglow lines, which vary from day to night and as a function of HST orbital position. The airglow lines may be the dominant sky contributions in the UV both for imaging-mode and spectroscopic observations. Away from the airglow lines, at wavelengths shortward of ~3000Å, the background is dominated by zodiacal light, where the small area of sky that corresponds to a pixel of the high resolution HST instrumentation usually produces a signal that is much lower than the intrinsic detector background. The contribution of zodiacal light does not vary dramatically with time and varies by only a factor of about three throughout most of the sky. Table 6.6 gives the variation of the zodiacal background as a function of ecliptic latitude and longitude. For a target near ecliptic coordinates of (50,0) or (-50,0), the zodiacal light is relatively bright at mv=20.9, i.e. about 9 times the faintest values of mv=23.3. Deep imaging applications must carefully consider expected sky values!

On the other hand, Earthshine varies strongly depending on the angle between the target and the bright Earth limb. The variation of the Earthshine as a function of limb angle from the sunlit Earth is shown in Figure 6.2. The Figure also shows the contribution of the moon, which is typically much smaller than the zodiacal contribution, for which the upper and lower limits are shown. For reference, the limb angle is approximately 24° when the HST is aligned toward its orbit pole (i.e., the center of the CVZ). The Earthshine contribution shown in Figure 6.1 and Table 6.8 corresponds to this position.

Figure 6.2: Background Contributions in V Magnitude per arcsec2 due to the zodiacal light, Moon, and the Sunlit Earth as a Function of Angle Between the Target and the Limb of the Earth or Moon. The two zodiacal light lines show the extremes of possible values.


 

For observations taken longward of 3500Å, the Earthshine dominates the background at small (<22°) limb angles. In fact, the background increases exponentially for limb angles <22°. The background near the bright limb can also vary by a factor of ~2 on timescales as short as two minutes, which suggests that the background from Earthshine also depends upon the reflectivity of the terrain over which HST passes during the course of an exposure. Details of the sky background as it affects ACS, as well as STIS, are discussed by Shaw, et al. (STIS ISR 98-21). The impact of Earthshine on ACS observations is discussed by Biretta, et al., (ACS ISR 03-05).


Table 6.6: Approximate Zodiacal Sky Background as a Function of ecliptic latitude and ecliptic longitude (in V magnitudes per square arcsec)
Ecliptic Longitude (deg)
Ecliptic Latitude (deg)
0
30
60
90
180
22.1
22.7
23.2
23.3
145
22.4
22.9
23.3
23.3
110
22.3
22.9
23.3
23.3
50
20.9
22.2
22.9
23.3

Observations of the faintest objects may need the special requirement LOW-SKY in the Phase II observing program. LOW-SKY observations are scheduled during the part of the year when the zodiacal background light is no more than 30% greater than the minimum possible zodiacal light for the given sky position. LOW-SKY in the Phase II scheduling also invokes the restriction that exposures will be taken only at angles greater than 40 degrees from the bright Earth limb to minimize Earthshine and the UV airglow lines. The LOW-SKY special requirement limits the times at which targets within 60 degrees of the ecliptic plane will schedule, and limits visibility to about 48 minutes per orbit. The use of LOW-SKY must be requested and justified in the Phase I Proposal.

The ETC provides the user with the flexibility to separately adjust both the zodiacal (low, average, high) and Earthshine (shadow, average, high) sky background components in order to determine if planning for use of LOW-SKY is advisable for a given program. However, the absolute sky levels that can be specified in the ETC may not be achievable for a given target; e.g., as shown in Table 6.6 the zodiacal background minimum for an ecliptic target is mv = 22.4 which is still brighter than both the low and average options with the ETC. By contrast, a target near the ecliptic pole would always have a zodiacal=low background in the ETC. The user is cautioned to carefully consider sky levels as the backgrounds obtained in HST observations can cover significant ranges.

Geocoronal Emission and Shadow

Background due to geocoronal emission originates mainly from hydrogen and oxygen atoms in the exosphere of the Earth. The emission is concentrated in the four lines listed in Table 6.7. The brightest line is Lyman- at 1216Å. The strength of the Lyman- line varies between about 2 and ~30 kilo-Rayleighs (i.e., between 6.1x10-14 and 6.1x10-13 erg sec-1 cm-2 arcsec-2 where 1 Rayleigh = 106 photons sec-1 cm-2 per 4 steradian) depending on the position of HST with respect to the day-night terminator and the position of the target relative to the Earth limb. The next strongest line is the OI line at 1304Å, which rarely exceeds 10% of Lyman-. The typical strength of the OI 1304Å line is about 1 kilo-Rayleighs (which corresponds to about 2.85x10-14 erg sec-1 cm-2 arcsec-2) on the daylight side and about 75 times fainter on the night side of the HST orbit. OI 1356 Å and OI 2471 Å lines may appear in observations on the daylight side of the orbit, but these lines are ~10 times weaker than the OI 1304 Å line. The width of the lines also vary with temperature, the line widths given in Table 6.7 are representative values assuming a temperature of 2000 K.

Except for the brightest objects (e.g. planets), a filter or prism mode which does not transmit at Lyman- should be employed. To minimize geocoronal emission the special requirement SHADOW can be requested. Exposures using this special requirement are limited to roughly 25 minutes per orbit, exclusive of the guide-star acquisition (or reacquisition) and can be scheduled only during a small percentage of the year. SHADOW reduces the contribution from the geocoronal emission lines by roughly a factor of ten while the continuum Earthshine is set to zero. SHADOW requirements must be included and justified in your Phase I proposal (see the Call for Proposals).


Table 6.7: Geocoronal emission lines
Wavelength
(Å)
ID
Line Width (Å)
Intensity
Day
Night
kilo-
Rayleighs
erg s-1 cm-2 arcsec-2 kilo-
Rayleighs
erg s-1 cm-2 arcsec-2
1216
Ly-
0.04
~20
6.1 x 10-13
2
6.1 x 10-14
1304
OI
0.013
~2
5.7 x 10-14
0.013
3.8 x 10-16
1356
OI
0.013
~0.2
~5 x 10-15
~ 0.001
~3 x 10-17
2471
OI
0.023
< 0.2
<3  x 10-15
< 0.001
<1.5 x 10-17

6.5 Extinction Correction


Extinction can dramatically reduce the counts expected from your source, particularly in the ultraviolet. Figure 6.3 shows the average Av / E (B - V) values for our galaxy, taken from (Seaton, MNRAS, 187, 73P, 1979). Large variations about the average are observed (Witt, Bohlin, Stecher, ApJ, 279, 698, 1984).

Extinction curves have a strong metallicity dependence, particularly in the UV wavelengths. Sample extinction curves can be seen in Koornneef and Code, ApJ, 247, 860 1981 (LMC); Bouchet et al., A&A, 149, 330 1985 (SMC); and Calzetti, Kinney and Storchi-Bergmann, ApJ, 429, 582, 1994, and references therein. At lower metallicities, the 2200Å bump which is so prominent in the galactic extinction curve disappears; and Av / E (B - V) may increase monotonically at UV wavelengths.

Figure 6.3: Extinction versus Wavelength


 

6.6 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 the three channels and also to present interesting cases as they may arise with the use of ACS.

At some future date HST may be operated with only two gyros, hence causing additional spacecraft jitter and degardition of the effevtive PSF. See the Two-Gyro Handbook for detailed information. All text in this ACS Handbook assumes three-gyro control.

6.6.1 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 and a photometry box size of 11x11 pixels, and average sky values.

The ACS Exposure Time Calculator (ETC) gives a total exposure time of 4410 sec 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 5 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, there is time for two 1200 sec 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 5303 sec (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 6.1 gives the integral QTd/ as 0.0775, and the AB correction term can be retrieved from Table 10.1 as 0.040. According to Figure 4.10, a circular aperture of radius 0.3 arcsec (which has an area of 116 pixels, close to the 121 pixel box specified) encloses about 90% of the light from a star. The count rate is then 2.5x1011*0.0775*0.9*10-0.4(26.5+0.040) = 0.423 counts/sec, which agrees with the ETC-returned value of 0.42. The exposure time can then be found by using the equation

to give t=4172 sec, which is close to the ETC-derived value of 4410s. We have inserted the background rate from Table 6.1 (Bsky=0.055) and Table 6.5 (Bdet=0.0032) 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, 5x5) and using LOW-SKY. Dropping the aperture size to 5x5 at average sky which still encloses 81% of the light requires 1532 sec. Including both the smaller 5x5 box and LOW-SKY (Zodiacal=LOW, Earthshine=AVERAGE) using the ETC gives the required exposure time as only 1306 sec (using CR-SPLIT=1), or 1540 sec with CR-SPLIT=2. The LOW-SKY visibility per orbit is 47 minutes, which allows a total on-target exposure time of 2000 sec in one orbit with CR-SPLIT=2.

Note also that the count rate from WFPC2 would be 0.167 electrons/sec, a factor of 2.5 lower.

6.6.2 Example 2: SBC Objective Prism Spectrum of a UV Spectrophotometric Standard 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 could be found by dearchiving the STIS spectrum)?

The sensitivity peaks in the 1500-1600Å region. To find the count rate at 1537Å, inspection of Figure 5.22 gives the sensitivity of 9.9x1014 counts/sec per erg/cm2/s/Å. Multiplying by the stellar flux of 5.3587x10-14 gives 53.0 counts/sec, summed in the cross dispersion direction. For the fraction of light in the central pixel =0.31, the brightest pixel at 1437.6Å is 17.6 counts/sec/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-. For daytime Ly- intensity of 20kR=6.1x10-13 erg cm-2 s-1 arcsec-2, S'=1.7x1014 and d, the dispersion in Å/pixel, is 2.58. Therefore, the background count rate is 6.1x10-13*1.7x1014*0.0322/2.58 = 0.041 counts/sec/pixel. This value varies somewhat over the field, as the plate scale varies from the nominal 0.032 arcsec/pixel. For faint source spectroscopy, it is better to use PR130L, which is on a CaF2 substrate to block Ly-.

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

What signal to noise ratio is reached in three one orbit exposures (~2400s each) for M87, when using the WFC, F555W for one orbit each in the three VIS polarizers? Gain is 2, box size is 5x5 pixels, CR-SPLIT=2 and average sky.

If the M87 jet region has µV=17 mag/square arcsec, using the ETC with a flat continuum spectral distribution and an exposure time of 2400s (CR-SPLIT=2), gives S/N=131.6 for an observation with each VIS polarizer filter (which is an average of the polarizer at the 3 available position angles 0º, 60º and 120º). If the polarization P is 20%, then P*S/N = 26.3, so using

from Chapter 5, P/P = 0.031, or P=6.2x10-3, which is the error on the fractional polarization. The error on the position angle should be ~1.0º using the formula, again from Chapter 5, of

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

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

The equation from the Section  "Emission Line Source" 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 1216Å is 0.0009, from inspection of Figure 10.106. For a surface brightness of 40kR = 1.22x10-12 erg cm-2 s-1 arcsec-2 (See Geocoronal Emission and Shadow for conversion), the total counts per pixel are given by the following calculation:

2.23x1012*0.009*1.22x10-12*1216*(0.032)2*2000 = 61.0.

The background contributions are the detector dark of 1.2x10-5 counts/pixel/sec (which can be ignored in this case) and a sky background which is dominated by geocoronal Lyman-. During the daytime, the geocoronal background is 20kR, or 30.5 counts, while at night the background drops to one tenth of this, or 3.05 counts.

Finally, we calculate the signal to noise ratio for a 2x2 pixel resolution element: in the daytime, = 12.7, while at night, = 15.2

6.6.5 Example 5: Chronographic imaging of the Beta-Pictoris Disk

In the final example 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 R magnitude of 16 arcsec-2 at a distance of 6 arcsec 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 ACS Exposure Time Calculator and considering the case for the 3.0" occulting mask:

6.7 Tabular Sky Backgrounds


We provide a table of the "high" sky background numbers as plotted in Figure 6.1. See the text and the caption in Figure 6.1 for more details. These high sky values are defined as the earthshine at 38° from the limb and the high zodiacal light of mV = 22.1 mag arcsec-2.


Table 6.8: High Sky Backgrounds 
Wavelength
Earthshine
Zodiacal Light
Total
Background
Å
erg sec-1 cm-2Å-1 arcsec-2
erg sec-1 cm-2Å-1 arcsec-2
erg sec-1 cm-2Å-1 arcsec-2
1000. 2.41E-23 1.26E-28 2.41E-23
1100. 4.38E-22 1.02E-26 4.38E-22
1200. 4.01E-23 1.05E-25 4.02E-23
1400. 4.29E-25 2.50E-24 2.93E-24
1500. 4.16E-25 9.12E-24 9.54E-24
1600. 2.55E-25 2.30E-22 2.30E-22
1700. 7.89E-23 7.06E-21 7.14E-21
1800. 9.33E-23 1.50E-20 1.51E-20
1900. 4.39E-22 2.20E-20 2.24E-20
2000. 1.01E-21 3.49E-20 3.59E-20
2100. 1.60E-21 1.21E-19 1.23E-19
2200. 7.49E-22 2.16E-19 2.17E-19
2300. 3.32E-22 1.75E-19 1.75E-19
2400. 2.50E-22 1.79E-19 1.79E-19
2500. 2.39E-22 2.47E-19 2.47E-19
2600. 5.62E-22 2.93E-19 2.94E-19
2700. 6.77E-21 9.95E-19 1.00E-18
2800. 2.03E-21 2.82E-19 2.91E-19
2900. 4.32E-20 2.04E-18 2.08E-18
3000. 9.34E-20 1.20E-18 1.29E-18
3100. 2.07E-19 1.46E-18 1.67E-18
3200. 3.60E-19 2.25E-18 2.61E-18
3400. 6.40E-19 2.81E-18 3.45E-18
3500. 8.20E-19 2.73E-18 3.55E-18
3600. 1.06E-18 2.68E-18 3.74E-18
3700. 1.22E-18 3.25E-18 4.47E-18
3800. 1.23E-18 3.05E-18 4.28E-18
3900. 1.52E-18 3.27E-18 4.79E-18
4000. 2.38E-18 4.54E-18 6.92E-18
4250. 2.33E-18 4.48E-18 6.81E-18
4500. 2.78E-18 5.32E-18 8.10E-18
5000. 2.55E-18 4.92E-18 7.47E-18
5250. 2.69E-18 5.28E-18 7.97E-18
5500. 2.56E-18 5.20E-18 7.76E-18
5750. 2.56E-18 5.33E-18 7.89E-18
6000. 2.40E-18 5.11E-18 7.51E-18
6250 2.27E-18 4.94E-18 7.21E-18
6500. 2.20E-18 4.88E-18 7.08E-18
6750. 2.07E-18 4.69E-18 6.76E-18
7000. 1.90E-18 4.40E-18 6.30E-18
7250. 1.85E-18 4.34E-18 6.19E-18
7500. 1.73E-18 4.13E-18 5.86E-18
7750. 1.63E-18 3.95E-18 5.58E-18
8000. 1.57E-18 3.85E-18 5.42E-18
8250. 1.48E-18 3.68E-18 5.16E-18
8500. 1.37E-18 3.46E-18 4.83E-18
8750. 1.31E-18 3.36E-18 4.67E-18


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