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Aerospacehard

Autonomous Atmospheric Density Profiling Mission

Design and construct a high-aspect-ratio passive aerostat capable of maintaining a stable, altitude-controlled glide path while deploying a serialized data collection payload. You must model and demonstrate a mechanism for atmospheric buoyancy compensation that accounts for thermocline-induced lift fluctuations without active propulsion. The success metric is defined by the stability of the descent rate and the accuracy of the spatial mapping of simulated thermal currents.

Materials: Mylar sheets, lightweight balsa wood dowels, adhesive tape, high-tensile fishing line, small calibrated lead weights, and a digital barometer or inclinometer.

Deadline: October 3, 2026
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Background: NASA/ESA Hubble