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WPI AIAA Research Rocket for the Investigation of Recovery and Staging
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WPI AIAA Research Rocket (WARRIORS)
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Thermal, Telecommunication and Power Systems for a CubeSat
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Production of a Liquid Microjet
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Production of a Fluid Microjet Using Electrospray and Flow Focusing
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Optical Emission Study of a Pulsed Plasma Thruster
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Mechanical, Power, and Thermal Subsystem Design for a CubeSat Mission
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Mechanical, Power, and Thermal Subsystem Design for a CubeSat
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Mechanical, Power, and Propulsion Subsystem Design for a CubeSat
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Investigation of Plasma Charging Effects
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Experimental and Computational Investigation of a Dual-Bell Nozzle
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Diagnostics for a Supersonic Wind Tunnel
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Development of a Plasma Source with Particulate Injector and Charging Sensor
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Design of a Supersonic Wind Tunnel
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Design and Test of a Radio-Frequency Electrothermal Thruster
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Design and Integration of a High-Powered Model Rocket-II
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Design and Integration of a High-Powered Model Rocket – III
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Design and Fabrication of a Radio-Frequency Electrothermal Thruster
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Design and Construction of a Supersonic Wind Tunnel
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Design and Analysis of the Sphinx-NG CubeSat
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