# Mitigating radiation damage of single photon detectors for space   applications

**Authors:** Elena Anisimova, Brendon L. Higgins, Jean-Philippe Bourgoin, Miles, Cranmer, Eric Choi, Danya Hudson, Louis P. Piche, Alan Scott, Vadim Makarov,, and Thomas Jennewein

arXiv: 1702.01186 · 2017-10-13

## TL;DR

This study evaluates the radiation effects on single-photon detectors for space, demonstrating that deep cooling and thermal annealing can effectively mitigate increased dark count rates caused by proton radiation.

## Contribution

It provides experimental data on radiation tolerance of avalanche photodiodes and photomultiplier tubes, and shows effective mitigation techniques for space-based quantum communication.

## Key findings

- Dark count rate increases significantly after proton irradiation.
- Deep cooling reduces dark count rate below operational thresholds.
- Thermal annealing further decreases dark count rate.

## Abstract

Single-photon detectors in space must retain useful performance characteristics despite being bombarded with sub-atomic particles. Mitigating the effects of this space radiation is vital to enabling new space applications which require high-fidelity single-photon detection. To this end, we conducted proton radiation tests of various models of avalanche photodiodes (APDs) and one model of photomultiplier tube potentially suitable for satellite-based quantum communications. The samples were irradiated with 106 MeV protons at doses approximately equivalent to lifetimes of 0.6 , 6, 12 and 24 months in a low-Earth polar orbit. Although most detection properties were preserved, including efficiency, timing jitter and afterpulsing probability, all APD samples demonstrated significant increases in dark count rate (DCR) due to radiation-induced damage, many orders of magnitude higher than the 200 counts per second (cps) required for ground-to-satellite quantum communications. We then successfully demonstrated the mitigation of this DCR degradation through the use of deep cooling, to as low as -86 degrees C. This achieved DCR below the required 200 cps over the 24 months orbit duration. DCR was further reduced by thermal annealing at temperatures of +50 to +100 degrees C.

## Full text

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## Figures

9 figures with captions in the complete paper: https://tomesphere.com/paper/1702.01186/full.md

## References

33 references — full list in the complete paper: https://tomesphere.com/paper/1702.01186/full.md

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Source: https://tomesphere.com/paper/1702.01186