Laboratory and Simulation Development for the AstroPIC Integrated Photonic Coronagraph
Direct characterization of potentially habitable terrestrial exoplanets around Sun-like stars requires extremely precise instrumentation capable of measuring a planet-star contrast ratio of 10-10. This instrumentation challenge pushes the limits of optical technology, with state-of-the-art coronagraphs requiring extremely precise wavefront control and large, complex, and expensive instrument designs. These bulk optics coronagraph instruments typically have limited measurable optical bandwidths and high sensitivity to the overall telescope pupil design (i.e. on-axis vs off-axis telescope configurations) and high sensitivity to optical aberrations. The AstroPIC project is applying programmable integrated photonics to develop a new kind of coronagraph instrument that is capable of reaching the theoretical limits of optimal coronagraph performance. This will result in a coronagraph instrument that is orders of magnitude smaller, less massive, and more flexible compared to traditional bulk optics designs, with the goal of increasing the Exo-Earth science yield of NASA’s Habitable Worlds Observatory flagship mission. The AstroPIC project is leveraging commercial silicon photonics fabrication to develop a coronagraph instrument that couples light from a telescope pupil plane into a mesh of integrated Mach-Zehnder interferometers on a photonic integrated circuit (PIC). The coupling is achieved by using a lenslet array to sample and focus the telescope pupil into an array of grating coupler waveguide inputs on the PIC, as shown in Figure 1a. Once the light from the telescope pupil is coupled onto the PIC, the interferometer mesh can be controlled by tuning thermal phase shifters in each interferometer to implement a mode-sorting algorithm in order to separate the starlight and planet light modes at high contrast levels. An integrated photonic testbed at NASA Ames Research Center is being developed to demonstrate coupling from a realistic telescope pupil into the PIC and will be used to characterize the contrast, throughput, and optical bandwidth of the coronagraph instrument. Figure 1b shows the design of the testbed, which will be used to experiment with different control algorithms for setting the tunable phase shifters in the photonic mesh and assess the factors limiting contrast on the chip to inform future iterations of the PIC design. Figure 1: (a) Diagram of AstroPIC instrument concept coupling the Habitable Worlds Observatory (HWO) pupil into an array of grating couplers using a microlens array. A mesh of Mach Zehnder Interferometers (MZIs) are tuned to separate starlight spatial modes from planet spatial modes. (b) Design of integrated photonics testbed under development at NASA Ames Research Center. The AstroPIC project has also developed simulations of the PIC coronagraph instrument concept in order to predict the coupling from the telescope pupil into the chip and simulate the photonic mesh behavior. Specifically, we are studying the application of the AstroPIC instrument concept to the NASA Habitable Worlds Observatory (HWO) flagship mission, which is currently in the pre-design phase. These simulations have shown that the AstroPIC concept is very robust to telescope pupil shape and aberrations for both on- and off-axis telescope configurations, and that the potential science yield of the AstroPIC coronagraph is very high even for relatively small numbers of input couplers. We find that the AstroPIC concept is particularly advantageous for accessing planets located at small inner working angles relative to the host star, which is extremely challenging for traditional coronagraph designs. Figure 2 shows these simulation results for an example HWO-like pupil, summarizing the predicted exo-Earth science yield as a function of (a) number of PIC input grating coupler channels, (b) starlight suppression order, and (c) end to end transmission efficiency. Figure 2: Predicted number of exo-Earths characterized over the HWO mission lifetime as a function of (a) number of input grating coupler PIC channels, (b) PIC starlight suppression order (number of output channels that are designated as starlight vs signal light), and (c) end-to-end transmission efficiency of the PIC instrument. These simulations are conducted using the FRIDAY yield calculation package.In this presentation, we will describe the AstroPIC instrument concept and how programmable photonics can be used to implement the optimal coronagraph operator. We will then present the development of an integrated photonics testbed at NASA Ames Research Center, which is being built to demonstrate the AstroPIC concept with a realistic telescope pupil directly coupled into the integrated photonic instrument. We will also review recent simulation results predicting the performance of next-generation AstroPIC instrument designs. Finally, we will discuss the next steps needed to mature this technology for future space telescope missions and ground telescope applications, including incorporating novel photonic component designs into the mesh architecture to improve the throughput and optical bandwidth of the instrument.
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