TPF-C Technology Plan - Exoplanet Exploration Program - NASA
TPF-C Technology Plan - Exoplanet Exploration Program - NASA
TPF-C Technology Plan - Exoplanet Exploration Program - NASA
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Chapter 1<br />
1.6.5 Sunshield<br />
The telescope is protected from the Sun by a six-vane v-<br />
groove radiator. This radiator rejects the heat from the Sun<br />
so that the telescope can rotate about its observing axis<br />
without significant deformation of the wavefront in the<br />
telescope. Extreme thermal stability is required so the<br />
optical wavefront will remain stable enough to allow for<br />
subtraction of the diffracted speckle pattern created by the<br />
telescope. The v-groove radiator is based on technology<br />
developed for the James Webb Space Telescope. The<br />
radiator must be deployed in space because it will not fit<br />
into a launch vehicle. Deployment from the stowed<br />
configuration behind the primary mirror is very challenging,<br />
requiring both radial and axial motion and tensioning of the<br />
thin vanes. The current concept for the sun shade<br />
deployment is shown in Figure 1-9.<br />
1.7 How <strong>TPF</strong>-C Detects <strong>Plan</strong>ets<br />
Figure 1-9. Concept for the<br />
<strong>TPF</strong>-C Deployable Sunshield<br />
<strong>TPF</strong>-C is designed as a high-performance coronagraph. The ability of <strong>TPF</strong>-C to detect a planet<br />
as separate from its host star is determined by the diffraction pattern of the primary mirror, as<br />
viewed through the optics of the coronagraph. There are two issues to contend with: (1) the<br />
primary mirror must be sufficiently large to provide the angular resolution necessary to resolve<br />
the planet as separate from the star, and (2) the sidelobes, stray light, and speckles in the<br />
diffraction pattern must be controlled and suppressed so that the faint planet light is detectable<br />
above the otherwise bright glare of the background.<br />
Diffraction effects are minimized by having an unobstructed primary mirror (using an off-axis<br />
telescope design) and requiring the mirror surface to be sufficiently flat at spatial scales<br />
corresponding to the angular separation of star and planet, thus reducing the halo of speckles<br />
arising from imperfections in the mirror itself.<br />
Scattered light is further controlled using two deformable mirrors that operate in concert to<br />
correct for both amplitude and phase irregularities in the wavefront. The remaining scattered<br />
light (after wavefront compensation) is blocked by a Lyot stop located in a pupil plane, and the<br />
diffraction pattern is further tapered using an image-plane stop.<br />
The key conflict arises that a larger telescope at least in principle improves the ability to separate<br />
the planet light from the star, because the planet will appear further away from the image of the<br />
star, but this makes the observatory larger, more technologically challenging, and more<br />
expensive. The principal design trade is therefore to arrive at a primary mirror diameter that<br />
does not impose unrealistic constraints on the coronagraph performance.<br />
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