David D. Smith,1 Andrew F. Heaton,1 Saba Ramazani,1 Daniel A. Tyler,1 Les Johnson,1 Charles Bachmann,2 Dylan J. Shiltz,2 Chris S. Lapszynski,2 Nayma B. Nurhttps://orcid.org/0000-0002-0039-9598,2 Chris H. Lee,2 Neset Akozbek,3 Dana Dement,4 Samuel Dummer,5 Brandon Farmer6
1NASA Marshall Space Flight Ctr. (United States) 2Rochester Institute of Technology (United States) 3U.S. Army Space and Missile Defense Command (United States) 4CFD Research Corp. (United States) 5Surface Optics Corp. (United States) 6NeXolve Corp. (United States)
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Reflectivity control devices (RCDs) based on polymer dispersed liquid crystals were fabricated for Solar Cruiser, a SmallSat NASA Pathfinder Mission consisting of a 1653 square meter solar sail that would establish an artificial orbit sunward of the L1 Lagrange point for heliophysics observations. Here we describe the optical characterization of these birefringent electro-optic devices including thin film measurements and analysis, hyperspectral bidirectional reflectance distribution function measurements, and radiometric analysis. These measurements demonstrate the promise of RCDs for roll control and momentum management of solar sails.
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David D. Smith, Andrew F. Heaton, Saba Ramazani, Daniel A. Tyler, Les Johnson, Charles Bachmann, Dylan J. Shiltz, Chris S. Lapszynski, Nayma B. Nur, Chris H. Lee, Neset Akozbek, Dana Dement, Samuel Dummer, Brandon Farmer, "Optical performance of reflectivity control devices for solar sail applications," Proc. SPIE PC12664, Optical Modeling and Performance Predictions XIII, PC1266405 (28 September 2023); https://doi.org/10.1117/12.2676775