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THERMAL AND STRUCTURAL ANALYSIS OF A ROCKETBORNE EXPERIMENT
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Six-Axis Monopropellant Propulsion System for Picosatellites
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Plume Analysis and Detection
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Nose Cone Design of an Aerial Drop Vehicle
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Hydrogen Peroxide Propulsion System for Nanosatellites
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Design of Setups for Plasma Propulsion Plume Experiments
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Design of Micropropulsion Plume Experiments
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Design of Microflow Experiments
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Design of a Plume Generation and Detection Systems
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Design of a micro-Pulsed Plasma Thruster for a 3U Cubesat
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Design and Integration of an Indoor Plume Experimental Setup
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Design and Integration of a High-Powered Model Rocket-I
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Design and Analysis of Subsystems for a CubeSat Mission
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Design and Analysis for the Sphinx-NG CubeSat
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Design and Analysis for CubeSat Missions
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Design and Analysis for a CubeSat Mission
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Design and Analysis for a CubeSat Mission
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Design and Analysis of a 6U Cubesat and Mission
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Magnetospheric Nanosat Design
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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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Design of a setup for plasma plume experiments
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Design of a NanoSat for an Ionospheric Mission
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Design of a 6U CubeSat for an Ionospheric Science Mission
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Design of a CubeSat for Identification of Space Debris
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