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TPF-I SWG Report - Exoplanet Exploration Program - NASA

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T E C H N O L O G Y R OADMAP FOR <strong>TPF</strong>-I<br />

Formation Flying (Multiple Robot Demonstration With Fault Recovery): Using the Formation<br />

Control Testbed, demonstrate that a formation of multiple robots can be safed following the injections of<br />

a set of typical spacecraft faults that have a reasonable probability of occurring during flight.<br />

Demonstrations can be limited to single-fault scenarios. This validates the software simulation of fault<br />

recovery for formation flight. Gate TRL 5.<br />

6.1.3 Cryogenic Technology Gate<br />

Cryocooler Development: With the Advanced Cryocooler Technology Development <strong>Program</strong>,<br />

demonstrate that the development model coolers meet or exceed their performance requirements to<br />

provide ~30 mW of cooling at 6 K and ~150 mW at 18 K. This demonstrates the approach to cooling the<br />

science detector to a temperature low enough to reveal the weak planet signals. Gate TRL 5. Completed<br />

Q2 2005.<br />

6.1.4 Integrated Modeling Gate<br />

Observatory Simulation: Demonstrate a simulation of the flight observatory concept that models the<br />

observatory subjected to dynamic disturbances (e.g., from reaction wheels). Validate this model with<br />

experimental results from at least the Planet Detection Testbed at discrete wavelengths. Use this<br />

simulation to show that the depth and stability of the starlight null can be controlled over the entire<br />

waveband to within an order of magnitude of the limits required in flight to detect Earth-like planets,<br />

characterize their properties, and assess their habitability. Gate TRL 5.<br />

6.2 Nulling Interferometry<br />

<strong>TPF</strong>-I is in Pre Phase A of its project life cycle, and its technology development is therefore directed at<br />

demonstrating the feasibility of the techniques that will be used. For starlight suppression it was thought<br />

impractical to demonstrate all that needed to be demonstrated on a single testbed. The effort has therefore<br />

been divided into tasks that can be addressed independently:<br />

1. Deep broad-band two-beam nulling;<br />

2. Planet detection with a four-beam nulling interferometer;<br />

3. Adaptive correction of amplitude and phase; and<br />

4. Suppression of higher-order wavefront modes using single-mode mid-infrared fiber optics.<br />

The requirements for the nulling testbeds from the 2005 technology plan are summarized in Table 6-2.<br />

6.2.1 State of the Art in Nulling Interferometry<br />

Progress in nulling interferometry is summarized in Figure 6-1. The plot shows rejection ratio as a<br />

function of bandwidth, for laboratory experiments that have been undertaken since 1998. On the far lefthand<br />

side of the plot are shown the results obtained using lasers at visible, near-infrared, and mid-infrared<br />

wavelengths. Experiments with bandwidths as large as 28% are shown. Results from ground-based<br />

observations of astronomical targets are not included; the rejection ratio obtained from experiments at<br />

telescopes have been less than 1000:1, dominated by atmospheric fluctuations. Of principal concern to<br />

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