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Completed TRL 3 (started at 3, targeting 4)
We propose a program to retire the key technical risk of far-infrared space astrophysics missions recently recommended by Astro2020. We will demonstrate large arrays of kinetic inductance detectors (KIDs) with the sensitivity and format required to deliver the massive scientific potential of spectroscopy aboard cryogenic space-borne observatories, whether a near-term probe-class facility like the Galaxy Evolution Probe (GEP) or a future Far-IR Great Observatory (FIRGO) similar to Origins. We will build on APRA development and ground-based and balloon-borne arrays to build packaged focal planes that can be directly inserted into phase A/B designs for these mission. We will demonstrate two arrays at wavelengths which bound the envisioned far-IR range: 25 μm and 350 μm, with pixel pitch, readout density, and size informed by these concept studies. Our two arrays will meet all of the essential performance and system-level requirements imposed by a near-term probe: 1. a per-pixel noise equivalent power (NEP) below 1×10^−19 W /sqrt(Hz). 2. provide ≥65% optical efficiency relative to a light incident on the pixel’s coupling optic, 3. can maintain high scientific utility in the face of cosmic-ray interactions in space, and 4. are packaged into a flight-ready housing with at least 8000 pixels demonstrating >80% yield and acceptable cross talk. KIDs are a strong choice for future far-IR observatories because they naturally enable the many-kilopixel arrays necessary for the wide-field spectral surveys. KIDs have demonstrated kilopixel arrays in a range of ground-based and balloon-borne missions, showing as-designed performance—background-limited for these platforms. Given recent developments in KID performance and detailed study for the Astro2020 mission studies, we are now ready to demonstrate KIDs for flight. We begin with the necessarily holistic design of the two arrays. Prior work provides a good understanding of the material properties and fabrication limitations, as well as demonstrations of 1000-pixel multiplexing. We will design the integrated low-volume KID inductor with the per-pixel concentrating optic (horn or microlens–a trade to be conducted early) to ensure good efficiency. Small subarray tests will be conducted early to vet the designs. Full array prototypes will follow to demonstrate yield as well as the key performance requirements, reading out four circuits simultaneously to show system-level operation and measure cross talk. Finally, we will design and build flight-worthy housings for the two arrays, assemble and subject them to vibration and particle testing, then re-verify performance to reach TRL-6. We submit that the current state of the technology is TRL 4, given fielded instruments meeting their requirements, and our work will position the large low-background far-IR KID arrays at TRL 6: ‘system demonstration in a relevant end-to-end environment.’ This work will be concurrent with the probe mission formulation, ensuring the suitability of the demonstrations for their purpose. The resulting prototype flight arrays will optimize scientific capability and clarify observatory interfaces. Our work will provide design rules for the other 2–4 far-IR wavebands at intermediate wavelengths. Demonstration of these arrays would be largely standard engineering and could be undertaken in project phase A/B.
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