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Design and Analysis of a High-Powered Model Rocket
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Optical Emission Study of a Pulsed Plasma Thruster
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WPI AIAA research rocket for the investigation and observations of recovery and staging (WARRIORS II)
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Design and Test of a Radio-Frequency Electrothermal Thruster
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Computational modeling of a hydrazine thruster
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WPI AIAA Research Rocket for the Investigation of Recovery and Staging
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Design and Fabrication of a Radio-Frequency Electrothermal Thruster
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Characterization of a field emission cathode
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CubeSat Component Thermal Modeling
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Design and Integration of a High-Powered Model Rocket – III
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Design and Integration of a High-Powered Model Rocket-II
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Investigation of Plasma Charging Effects
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Design and Analysis of the Sphinx-NG CubeSat
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Design and Construction of a Supersonic Wind Tunnel
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Mechanical, Power, and Thermal Subsystem Design for a CubeSat
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Diagnostics for a Supersonic Wind Tunnel
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Design, Analysis, and Test of a High-Powered Model Rocket-2
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Ice-cube mechanical properties for hail ingestion tests
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Internal leak testing of MEMS valve components for space applications
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Design of a Supersonic Wind Tunnel
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