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Design of Thermally Efficient Cryogenic Tanks for Spacecraft
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Novel Mobility Solutions for Extreme Lunar Terrain
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Design of a CubeSat 2324: Mechanical, Propulsion, Environment
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Design, Analysis and Testing of Ionic Wind Propulsion System for an Electric Aircraft
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Design, Fabrication, and Testing of Surface Undersea Kite Prototypes
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Coupled Sensor Configuration and Planning with Unmanned Aerial Vehicles
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CubeSat Development for Identification of Space Debris
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Structural Design Analysis of the Burnelli CBY-3 Loadmaster and DC-3
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Design of Thermally Efficient Cryogenic Tanks for Spacecraft
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Micro-Aircraft Design for 2022 SAE AeroDesign Competition
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