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Lunar Dielectric Analyzer (LDA) for the Artemis First Landing Mission: Instrument Design and Operational Concept for In Situ Permittivity Measurements

  • Authors: Makito Kobayashi, Hideaki Miyamoto, Airi Toida, Yuta Sugihara, Hiroki Aida, Tomohiro Takemura, Yuta Shimizu, Tetsuo Yoshimitsu

Makito Kobayashi et al 2026 The Planetary Science Journal 7 .

  • Provider: AAS Journals

Caption: Figure 3.

Operational flow of the LDA showing the sequence of autonomous operations under changing illumination conditions. After crew-assisted deployment and activation, the LDA operates autonomously using System A during the initial sunlit phase while the HLS remains on the surface. Following depletion of the primary battery, the system transitions autonomously to System B for extended operations. During sunlit periods, System B conducts autonomous dielectric measurements powered by the SAP. When solar illumination becomes unavailable, the system automatically powers off, and upon re-illumination, it autonomously powers on and resumes measurements and communication, enabling long-term, crew-independent operation across multiple illumination cycles. “Artificial shadow” denotes shadow cast by the HLS or the protective assembly during the illuminated lunar day, under which System A performs dielectric measurements. Under nominal deployment conditions, this shadow is expected to last for at least approximately 5 hr, although its actual duration depends on the deployment geometry and local solar illumination conditions. “Shadow (night)” denotes the true lunar night, during which System B does not acquire data due to the absence of solar power.

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