Research

Current/LUSEM
LUSEM

LUSEM

LUnar Space Environment Monitor

Lunar Space Environment Monitor (LUSEM) is a lunar-surface space-environment instrument developed to characterize energetic charged-particle conditions near the Moon and how they vary with location and upstream conditions. The payload is planned to operate on the lunar nearside in the Reiner Gamma swirl region, a scientifically distinctive area associated with localized magnetic anomalies and unusual surface albedo patterns.


Fig 1. Reiner Gamma overview (credit: NASA's Scientific Visualization Studio)


By measuring the near-surface particle environment, LUSEM supports Artemis-era lunar exploration by improving our understanding of radiation exposure and plasma–surface interactions in a real lunar setting. The instrument is composed of a sensor head (LSH) and an integrated data-processing unit (IDPU) designed for autonomous observation and robust data handling in a resource-constrained surface mission.


Fig 2. Operating Principle of the LUSEM Sensor Head(LSH)


Ultimately, LUSEM aims to provide an observational basis for linking local lunar environments to broader heliospheric drivers and to the Moon’s interaction with Earth’s magnetospheric tail.


SSIL contributed across the end-to-end development chain with a practical focus on turning an on-surface measurement concept into a usable scientific dataset. A key component of SSIL’s work was direct contribution to detector fabrication, including hands-on support for building and assembling detector elements and associated hardware needed to realize the sensor head. SSIL also supported engineering verification activities that connect fabricated hardware performance to mission-relevant data quality, helping define checks for basic functionality, stability, and measurement consistency under representative operational conditions. In parallel, SSIL prepared analysis-side foundations—defining data products at a level suitable for scientific interpretation and outlining processing steps that preserve traceability from raw measurements to higher-level observables. Where appropriate within public scope, SSIL’s role can be summarized as bridging “hardware realization” and “science readiness,” ensuring that detector build outcomes, test results, and data interpretation needs remain aligned throughout the project lifecycle.


LUSEM’s system concept separates sensing and onboard processing into two major blocks: the LSH provides the particle-measurement front end, while the IDPU provides instrument control, data acquisition, and packaging for downlink and subsequent analysis. The measurement approach is centered on capturing energetic charged-particle signatures near the lunar surface and organizing them into time-tagged products that can be compared across environmental conditions and observation periods. The Reiner Gamma site offers a compelling context for these observations because swirl regions and magnetic anomalies raise well-known questions about how local electromagnetic conditions may influence surface weathering and the near-surface plasma environment.

At the mission level, LUSEM is intended for delivery through NASA’s Commercial Lunar Payload Services (CLPS) initiative, leveraging a commercial lander platform to enable surface operations and continuous monitoring over an operational window.




Fig. 3. CLPS commercial lunar lander (Nova-C) illustration (credit: Intuitive Machines)


To interpret variability, LUSEM observations are framed against large-scale space-environment drivers, including whether the Moon is inside or outside Earth’s magnetotail, which can modulate particle access and background conditions.


The project’s most important outcome is the establishment of a lunar-surface measurement capability for energetic particle conditions in a scientifically unique nearside region, with an instrument architecture designed for reliable acquisition and scientifically interpretable outputs. SSIL’s detector fabrication contribution strengthens the project’s hardware readiness by ensuring that the sensing chain is realized in buildable, testable form and that fabrication feedback informs verification and data-quality planning. A second outcome is science readiness: the definition of data products and processing viewpoints that allow surface measurements to be translated into interpretable trends, comparisons, and contextual analyses without over-reliance on mission-specific assumptions. As mission operations proceed, these foundations support the production of consistent datasets that can be used to study near-surface energetic particle behavior, location-dependent differences, and broader environmental modulation relevant to future lunar exploration activities.