Technical Instrument Report WFPC2 97-01 Results of the WFPC-2 SMOV Relative Photometry Check (prop-ID 7020) B. Whitmore, S. Gonzaga, I. Heyer December 1, 2008 ABSTRACT The photometric throughput of the WFPC2 was essentially unaffected by the 1997 servicing mission. The mean change in throughput is observed/predicted = 0.9984 +/- 0.0023. The largest deviation is a decline of 0.4 +/- 0.2% in the PC1. Even this should be considered tentative until new observations become available during the next few months, since it represents only a 2-sigma deviation. 1. Introduction The second HST Servicing Mission (SM97) concluded February 18, 1997. During this mission STIS, NICMOS, and various other components were installed. While WFPC2 was not serviced, it is still important to ensure that neither the astronaut activities nor contamination from any other source, such as the installment and subsequent powering up of new instruments, altered the performance of WFPC2. Herein we describe the procedure and results for the WFPC2 relative photometry check (proposal 7020). The goal of the relative photometry check was to verify that the photometric accuracy remained unchanged at the 1-2% level. Our regular photometric standard star, GRW+70D5824, was observed in a variety of filters (F160BW, F170W, F185W, F218W, F255W, F300W, F336W, F439W, F555W, F675W, and F814W) on March 5, 1997 (MJD 50512), with the star centered in each of the 4 CCDs (one orbit per CCD). Each orbit started with an observation with the F555W filter in the PC1, in order to monitor any drifts in the throughput. This program was run one day after the “protect decon” which executed 13 days after HST release from the shuttle. WFPC2 was at its normal operating temperature of -88C. The results were compared to observations of the same object taken prior to the servicing mission. 1 2. Procedure Photometric count rates were measured independently by using two methods, using pipeline-calibrated data. Method #1 used IRAF scripts developed by Christine Ritchie for routine photometric monitoring of WFPC2 over the past several years. Method #2 used more automated IRAF scripts developed by Whitmore and Heyer (script_smov_7020 to be found at /data/rainier1/smov). Both cases used an aperture radius of 0.5 arcsecs (5 pixels in the WF chips; 11 pixels in the PC1 chip) for the targets, and an annulus from radius 30 to 35 pixels for determining the sky values. The agreement between both methods was very good (method #1 / method #2 = 0.9993 +/- 0.0002). The values from method #1 were used for the comparative analysis, since this method was also used to establish the baseline measurements. The baseline measurements have been corrected for contamination using the contamination rates in ISR WFPC2 96-04. Figures 1a -1i show the baseline observations over roughly the past 2 years (since MJD = 49750, i.e. Feb. 2, 1995) and the March 5, 1997, observations from proposal 7020 for the full set of filters and chips. The measurements have been normalized to a mean of 1.000 based on the baseline observations. The 1-sigma scatter (based on the empirical scatter) of the baseline measurements are shown by dashed lines. In cases with less than 10 baseline measurements (i.e. WF2 and WF4 for all but F170W), the scatter from WF3 has been adopted. In cases where no baseline measurements were available the value on WF3 was used. The observations were taken on March 5, 1997 (MJD 50512.22 to 50512.44), roughly one day after a decontamination (MJD 50511.43). One observation with the F255W filter in the WF3 chip was excluded from the analysis because the star’s central pixel was saturated. A contamination rate of 1.7 times the pre-SMOV values has been adopted, based on measurements from proposal 7016 (see forthcoming TIR). The contamination correction is very small in all cases (maximum of 1.3% for F160BW on WF4), since the observations were taken within 1 day of the decontamination. The observed scatter in the F555W observations on the PC1 taken at the start of each orbit is less than the predicted scatter, hence no correction for a “drift” from orbit to orbit was made. Figures 1a-1i show that in all cases the observed count rates from March 5, 1997, are in good agreement with pre-SMOV data, showing that WFPC2 throughput was essentially unaffected by the 1997 servicing mission. A flat mean has been adopted in all cases, except for F160BW and F170W on the PC1 chip, where a slow increase in the throughput as a function of time has been observed previously (see ISR WFPC2 96-4). For these two cases a linear fit was adopted, using baseline data, to predict the value for March 5, 1997. 2 Figures 2a and 2b show the observed versus predicted values for all cases with more than 10 baseline measurements (N=22 in the resulting sample) both in terms of the ratio of observed to predicted values, and as the 1-sigma scatter (shown as dashed lines in Figures 1a - 1i). Overall, the agreement is excellent, with only a very small (1 sigma) hint that the throughput has decreased by about 0.16% (i.e. observed/predicted = 0.9984 +/- 0.0023). However, there is some evidence for a slightly larger effect on the PC1 alone, at about the 2-sigma level (i.e. N=12, observed/predicted = 0.9958 +/- 0.019 for the PC1, N=8, observed/predicted = 1.0010 +/- 0.015 for the WF3). Including all the data (i.e. chips WF2 with two baseline observations and WF4 with five baseline observations) yields a value of observed/predicted = 0.9968 +/- 0.0026. Table 1 shows the numbers from the analysis (from the file /data/rainier1/smov/ final_7020_shireen_brad.dat). It is interesting to note that the observed value of the scatter is less than the predicted scatter (i.e. the width in Figure 2a is 0.64, less than 1.0). This indicates that there is more structure in the long-term baseline data than just random Gaussian noise. Examples can be seen in the F170W WF3 and F218W WF3 baseline observations (Figures 1b and 1c), where the throughput during days 49750-50000 appears to be about 3% higher than the more recent observations. Table 1: Proposal 7020 WFPC2 Photometry Check Results Pre - SM97 Baseline File Filter Chip N Post - SM97 predicted (DN/sec) sigma(DN/sec) Mar.5 (DN/sec) U3SG0101R F555W 1 61 3744.80 41.36 3708.52 2R F170W 1 64 164.24 1.75 163.80 3R F160BW 1 27 84.22 3.73 84.09 5R F218W 1 27 140.16 2.63 138.78 6R F255W 1 27 160.75 2.02 158.26 7R F336W 1 27 773.33 9.98 773.24 8R F439W 1 36 894.33 9.14 901.99 9R F675W 1 27 2103.52 17.24 2093.15 AR F814W 1 43 1359.81 15.25 1358.94 U3SG0201R F555W 1 61 3744.80 41.36 3701.69 2R F160BW 2 2 79.16 2.24 76.22 3R F170W 2 12 192.37 3.78 191.99 4R F218W 2 1 141.67 3.47 145.90 3 Post - SM97 Pre - SM97 Baseline File Filter Chip N predicted (DN/sec) sigma(DN/sec) Mar.5 (DN/sec) 5R F255W 2 2 169.13 3.27 164.78 7R F336W 2 2 789.06 13.02 784.19 8R F439W 2 2 905.09 7.57 909.61 9R F555W 2 2 3811.86 34.08 3787.27 AR F675W 2 0 INDEF 18.23 2153.77 BR F814W 2 2 1393.16 18.24 1388.03 U3SG0301M F555W 1 61 3744.80 41.36 3735.94 2R F160BW 3 23 69.21 2.24 71.37 3R F170W 3 61 160.30 2.88 158.58 4R F218W 3 24 135.97 3.47 134.26 6R F336W 3 24 800.19 13.02 790.90 7R F439W 3 23 893.60 7.57 887.34 8R F555W 3 24 3818.50 34.09 3822.54 9R F675W 3 18 2087.88 18.23 2093.15 AR F814W 3 24 1359.79 18.25 1380.38 U3SG0401R F555W 1 61 3744.80 41.36 3746.28 2R F160BW 4 5 72.80 2.24 70.45 3R F170W 4 13 169.84 3.57 171.48 4R F218W 4 0 INDEF 3.47 144.04 5R F255W 4 5 168.69 3.27 167.44 6R F336W 4 5 786.98 13.02 817.72 7R F439W 4 5 892.54 7.57 889.03 8R F555W 4 5 3829.37 34.08 3756.38 9R F675W 4 0 INDEF 18.23 2097.01 AR F814W 4 5 1379.88 18.25 1366.47 3. Summary The throughput of WFPC2 was essentially unaffected by the 1997 servicing mission. The mean change in throughput is observed/predicted = 0.9984 +/- 0.0023. There is a slight (2-sigma) tendency for the PC1 chip to be 0.4% lower following the servicing mission. This result should be considered tentative until new observations become available during the next few months. 4 Figure 1a: F160BW 5 Figure 1b: F170W 6 Figure 1c: F218W 7 Figure 1d: F255W 8 Figure 1e: F336W 9 Figure 1f: F439W 10 Figure 1g: F555W 11 Figure 1h: F675W 12 Figure 1i: F814W 13 Figure 2a: Observed vs Predicted Values 14 Figure 2b: Distribution in terms of Sigma 15