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WPI AIAA research rocket for the investigation and observations of recovery and staging (WARRIORS II)
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Internal leak testing of MEMS valve components for space applications
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Characterization of a field emission cathode
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Analysis and design of a total temperature probe
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Design and Construction of a Supersonic Wind Tunnel
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Development of a Plasma Source with Particulate Injector and Charging Sensor
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Mechanical, Power, and Thermal Subsystem Design for a CubeSat Mission
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Production of a Fluid Microjet Using Electrospray and Flow Focusing
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Production of a Liquid Microjet
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Thermal, Telecommunication and Power Systems for a CubeSat
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