Ground Testing and Flight Demonstration of Charge Management of Insulated Test Masses Using UV LED Electron Photoemission
Shailendhar Saraf, Sasha Buchman, Karthik Balakrishnan, Chin Yang Lui,, Michael Soulage, Dohy Faied, John Hanson, Kuok Ling, Belgacem Jaroux,, Abdullah AlRashed, Badr Al Nassban, Badr Al Suwaidan, Mohammed Al Harbi, Badr, Bin Salamah, Mohammed Bin Othman, Bandar Bin Qasim

TL;DR
This paper reports on the successful ground testing and space demonstration of UV LED-based charge management for isolated test masses, advancing space accelerometer technology with improved control and durability.
Contribution
It introduces UV LEDs operating at 255 nm for charge management, demonstrating their advantages over traditional mercury lamps and achieving high TRL levels in space.
Findings
UV LEDs outperform mercury lamps in size, power, and control.
Successful in-orbit control of test mass potential over 20 mm gap.
UV LED performance remains stable after 12 months in orbit.
Abstract
The UV LED mission demonstrates the precise control of the potential of electrically isolated test masses that is essential for the operation of space accelerometers and drag free sensors. Accelerometers and drag free sensors were and remain at the core of geodesy, aeronomy, and precision navigation missions as well as gravitational science experiments and gravitational wave observatories. Charge management using photoelectrons generated by the 254 nm UV line of Hg was first demonstrated on Gravity Probe B and is presently part of the LISA Pathfinder technology demonstration. The UV LED mission and prior ground testing demonstrates that AlGaN UV LEDs operating at 255 nm are superior to Mercury vapor lamps because of their smaller size, lower draw, higher dynamic range, and higher control authority. We show flight data from a small satellite mission on a Saudi Satellite that demonstrates…
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