Simulating the charging of isolated free-falling masses from TeV to eV energies: detailed comparison with LISA Pathfinder results

TL;DR

This paper presents a detailed model of test mass charging in the LISA Pathfinder mission, combining particle tracking from TeV to eV energies with electrostatic simulations, to explain observed charging behavior and noise contributions.

Contribution

The study introduces a comprehensive simulation approach integrating high- and low-energy particle tracking with electrostatic modeling, providing new insights into test mass charging mechanisms.

Findings

Model accurately reproduces observed charging rates

Low-energy electrons contribute ~10% to net charging

Electrons significantly increase charging-current noise by ~40%

Abstract

A model is presented that explains the charging rate of the LISA Pathfinder test masses by the interplanetary cosmic ray environment. The model incorporates particle-tracking from TeV to eV energies using a combination of GEANT4 and a custom low-energy particle generation and tracking code. The electrostatic environment of the test mass is simulated allowing for a comparison of the test-mass charging-rate dependence on local electric fields with observations made in orbit. The model is able to reproduce the observed charging behavior with good accuracy using gold surface properties compatible with literature values. The results of the model confirm that a significant fraction of the net charging current is caused by a population of low-energy ($\sim$eV) electrons produced by electron- and ion-induced kinetic emission from the test mass and surrounding metal surfaces. Assuming a gold work function of 4.2 eV, the unbalanced flow of these electrons to and from the unbiased test mass contributes $\sim$10% of the overall test mass charging rate. Their contribution to the charging-current shot noise is disproportionately higher and it adds $\sim$40% to the overall predicted noise. However, even with this increased noise contribution the overall charging-current noise is still only 40% of that measured in-orbit, and this remains an unsolved issue.