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TPF-I SWG Report - Exoplanet Exploration Program - NASA

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C HAPTER 5<br />

30<br />

25<br />

5 M earth<br />

3 M earth<br />

All (1014)<br />

<strong>TPF</strong>-C [75 - 100%] (26)<br />

<strong>TPF</strong>-C [50 - 75%] (24)<br />

<strong>TPF</strong>-C [25 - 50%] (27)<br />

<strong>TPF</strong>-C [0 - 25%] (17)<br />

<strong>TPF</strong>-I [90%] (240)<br />

Series7<br />

10 M earth<br />

SIM (100 stars)<br />

Distance / pc<br />

20<br />

15<br />

2 M earth<br />

10<br />

Sun @ 10 pc<br />

5<br />

1 M earth<br />

0<br />

301 605<br />

0 50 100 150 200<br />

Projected radius of Inner Habitable Zone / mas<br />

Figure 5-22. Comparison of <strong>TPF</strong>-I, <strong>TPF</strong>-C, and SIM Missions. The colored circles represent those stars<br />

for which an Earth-sized planet could be detected in the Habitable Zone by the <strong>TPF</strong>-C mission. The color<br />

indicates the completeness of the measurement, as indicated in the legend. For example, the yellow<br />

symbols show stars for which there is a probability of between 50 and 75% that a given Earth-sized<br />

planet in the habitable zone is detected. There are 24 such stars. The completeness diminishes with<br />

distance and proximity of the habitable zone to the star. The circles with a heavy outline denote the 240<br />

stars that can be surveyed for Earth-sized planets in the habitable zone with 90% completeness by the<br />

<strong>TPF</strong>-I mission. The blue contours represent the planet mass sensitivity of the SIM mission for an Earthequivalent<br />

orbit. The astrometric signature is proportional to the mass of the planet and the projected orbit<br />

radius, and inversely proportional to the mass of the parent star. For a star lying on the 3-Earth-mass<br />

contour, there is a 50% probability that a given 3-Earth-mass planet will be detected.<br />

The spectroscopy observations are made in exactly the same manner as for detection and orbit<br />

determination: that is, the array is rotated continuously about the line of sight to the star and<br />

measurements are made “on-the-fly.” Many rotations may be needed to accumulate the necessary<br />

integration time. Efficiency (integration time/mission time) is assumed to be 75%.<br />

Figure 5-23 shows how the SNR in a 0.5-μm wide channel varies with wavelength, for an integration time<br />

of 29 days on an Earth-sized planet at 15 pc. Much of the variation in SNR (Fig. 5-23b) can be attributed<br />

to the variation in signal photon rate from the planet (modeled as a 265-K black body as shown in Fig. 5-<br />

23a). The SNR is reduced at short wavelengths by the increase in stellar leakage, since the width of the<br />

null is proportional to the wavelength. At long wavelengths the SNR is depressed by the increase in<br />

122

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