TPF-I SWG Report - Exoplanet Exploration Program - NASA
TPF-I SWG Report - Exoplanet Exploration Program - NASA
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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