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Lunar Vehicle Active Charge Control System (LVACCS)+The Lunar Vehicle Active Charge Control System (LVACCS) is an instrument in development that will measure the electrical potential of a spacecraft or rover under both positive and negative charge conditions, actively discharge negative charge, and charge the vehicle to a safe positive potential. All surfaces immersed in a plasma charge to non-zero potentials. In very low-density plasma (< 100 cm^-3), space vehicle charging can interfere with plasma probe measurements, degrade avionics performance, or cause a total system failure. LVACCS provides real-time in-situ space situational awareness that overcome these challenges in a small package. LVACCS has been awarded a NASA PICASSO grant to bring the instrument to technology readiness level 5. LVACCS consists of two main components: a collimated photoelectron gun (CPEG) and a Spacecraft Charge Detector (SCD).Monitoring charge build up on the lunar surface isa critical first step to understand hazards for crew, rovers, and instrumentation operating there.The LVACCS instrument will be able to fill in this gap providing robust lunar surface potential measurements and active charge dissipation.
Document ID
20240012820
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Heidi Fuqua Haviland
(Marshall Space Flight Center Redstone Arsenal, United States)
Omar Leon
(University of Michigan–Ann Arbor Ann Arbor, United States)
Linda Habash Krause
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
October 7, 2024
Publication Date
September 27, 2024
Publication Information
Subject Category
Lunar and Planetary Science and Exploration
Meeting Information
Meeting: LuPIN 2 Conference (Lunar Plasma Interdisciplinary Network)
Location: Storforsen
Country: SE
Start Date: September 23, 2024
End Date: September 27, 2024
Sponsors: European Space Agency, ESTEC
Funding Number(s)
WBS: 811073.02.52.01.47
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
Single Expert
Keywords
Moon
plasma
instrument
geophysics
surface charging
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