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WPI AIAA Research Rocket (WARRIORS)
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An Experimental Investigation of Aerodynamic Drag on a Round Parachute Canopy
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A microscale mass-flow measuring system
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Analysis and design of a total temperature probe
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Analysis of a micro-retarding potential analyzer
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Analysis of an onboard infrared camera assembly
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Computational modeling of a hydrazine thruster
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Experiments on trailing edge notches for MAVs
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Fluid flow modeling in a Stirling engine using the ultra HI-FI method
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Internal leak testing of MEMS valve components for space applications
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