18 citations as recorded by crossref.

1. The Solar Probe Plus Radio Frequency Spectrometer: Measurement requirements, analog design, and digital signal processing M. Pulupa et al. 10.1002/2016JA023345
2. SPIS 5.1: An Innovative Approach for Spacecraft Plasma Modeling B. Thiebault et al. 10.1109/TPS.2015.2425300
3. Plasma potential in the sheaths of electron‐emitting surfaces in space X. Wang et al. 10.1002/2015GL067175
4. Retrieving True Plasma Characteristics from Langmuir Probes Immersed in the Spacecraft Sheath: The Double Hemispherical Probe Technique J. Samaniego & X. Wang 10.1029/2019JA027176
5. Parker Solar Probe FIELDS Instrument Charging in the Near Sun Environment: Part 2: Comparison of In‐Flight Data and Modeling Results M. Diaz‐Aguado et al. 10.1029/2020JA028689
6. Verifying effects of instability enhanced ion–ion Coulomb collisions on ion velocity distribution functions near the sheath edge in low temperature plasmas C. Yip et al. 10.1088/0963-0252/24/1/015018
7. Electrostatic Potential Shielding in Representative Cislunar Regions K. Champion & H. Schaub 10.1109/TPS.2023.3236246
8. Correcting Parker Solar Probe Electron Measurements for Spacecraft Magnetic and Electric Fields D. McGinnis et al. 10.1029/2019JA026823
9. Parker Solar Probe FIELDS Instrument Charging in the Near Sun Environment: Part 1: Computational Model M. Diaz‐Aguado et al. 10.1029/2020JA028688
10. Frequency range of dust detection in space with radio and plasma wave receivers: Theory and application to interplanetary nanodust impacts on Cassini N. Meyer‐Vernet et al. 10.1002/2016JA023081
11. A Study of Solar Orbiter Spacecraft–Plasma Interactions Effects on Electric Field and Particle Measurements S. Guillemant et al. 10.1109/TPS.2017.2731054
12. SPIS 5: New Modeling Capabilities and Methods for Scientific Missions P. Sarrailh et al. 10.1109/TPS.2015.2445384
13. Sheath-induced distortions in particle distributions near enhanced polar outflow probe particle sensors S. Hussain & R. Marchand 10.1063/1.4887257
14. Simulation Study of Spacecraft Electrostatic Sheath Changes With the Heliocentric Distances From 0.044 to 1 AU S. Guillemant et al. 10.1109/TPS.2013.2246193
15. Development of a comprehensive physics-based model for study of NASA gateway lunar dust contamination R. Lee et al. 10.1016/j.actaastro.2023.05.025
16. Spacecraft charging analysis with the implicit particle-in-cell code iPic3D J. Deca et al. 10.1063/1.4826951
17. The FIELDS Instrument Suite for Solar Probe Plus S. Bale et al. 10.1007/s11214-016-0244-5
18. Cross-comparison of spacecraft-environment interaction model predictions applied to Solar Probe Plus near perihelion R. Marchand et al. 10.1063/1.4882439