Jaeheon Cheong

The authors have made the following corrections to the author list and the content of the original publication

CubeSat programs are often conducted under severe constraints in budget, personnel, schedule, and knowledge continuity, while still requiring sufficient verification to support mission success. This paper presents the verification, testing, on-orbit operation, and anomaly analysis of COSMIC, a 3U CubeSat jointly developed by Yonsei University, Unmanned Exploration Laboratory (UEL), and UZURO Tech Inc. in less than eleven months from project kickoff to launch. COSMIC adopted a protoflight model approach, prioritized commercial off-the-shelf components with flight heritage and prior laboratory experience, and concentrated limited resources on subsystem, FlatSat, system-level, environmental, communication, and scenario-based testing. The test program is reviewed against the subsequent on-orbit results to identify which verification activities contributed to anomaly prevention, fault isolation, and recovery. The results show that system-level integration testing, thermal vacuum cycle testing, and scenario testing were particularly effective in revealing interface, software, and deployment-related issues before launch and in supporting early orbit recovery. However, the mission also exposed limitations in recovery-logic verification, long-duration software testing, communication robustness, and independent reset paths. Based on these findings, practical recommendations are derived for resource-constrained CubeSat teams seeking to tailor verification activities without simply reducing test rigor.

CubeSats operating under nadir-pointing or mission-priority attitude conditions often experience unfavorable solar incidence on their solar panels, limiting available onboard power. This study proposes a thermally driven passive sun-pointing mechanism for CubeSat solar panels and evaluates its prototype-level feasibility. The mechanism uses a photothermal panel, heat pipe, heat cartridge, shape memory alloy (SMA) spring, and universal joint to convert external thermal input into panel tilting motion without direct electrical actuation. A prototype was evaluated through SMA spring actuation tests, single-module pointing experiments, four-direction pointing tests, orbital thermal analysis, and expected annual energy-generation analysis. The experiments showed thermally induced contraction and recovery tendency of the two-way SMA spring and demonstrated that selective thermal input can generate directional tilting and return motion in a four-direction prototype. Orbital thermal analysis indicated that heat can be transferred to the actuation region while maintaining directional thermal separation. The energy-generation analysis suggested that limited-angle pointing can improve annual energy generation compared with a fixed flat panel. These results support the prototype-level feasibility of the proposed mechanism, although further multi-axis measurement, long-term cycling, and thermal-vacuum validation are required.