Student Number : 0105159R - MSc(Eng) Dissertation - School of Electrical and Information Engineering - Faculty of Engineering and the Built Environment / This dissertation presents the design of a re-usable rocket for use in triggered-lightning experiments. It is intended that the rocket will tow a thin wire to sufficient height so that the lightning mechanism will attach onto the wire and follow it to ground. The rocket design is inherently safe as it does not use explosive materials for its propulsion system, and hence conforms to South African explosive legislation. The designed rocket consists of a hybrid motor, which uses a solid combustion chamber and liquid oxidiser rather than solid motors which use a single solid fuel or a liquid motor which uses two liquid propellants. The mechanical performance of the oxidiser stage is critical in containing the pressurised oxidiser and regulating the flow of the oxidiser into the combustion chamber. The design of the combustion chamber and the rate at which the solid material burns is key to the generation of the pressure which is expelled through the nozzle to produce thrust. The design of the nozzle is covered in which the material from which it is made must withstand temperatures in excess of 1600 ◦C. The entire system was modelled to calculate the parameters of the various subsystems. The simulation study shows that the rocket will be able to reach 1 km with a complete section of wire towed behind it. A cost analysis, against other commercial rocket systems, was performed. The analysis concludes from the total cost of ownership that it is significantly cheaper to operate the designed rocket, over the course of the experiment, than other rocket systems.

Additively manufactured fuels are becoming more common in the area of hybrid rockets due to the enhanced possibilities provided by computer aided design and improved additive material technology. When integrated with a highly compliant yet energetic paraffin wax, the additive manufactured material can help support the paraffin wax during the burn, and improve overall performance. This study investigates thin-walled acrylonitrile butadiene styrene structures that separate paraffin wax into azimuthally partitioned cells. The fuel grains are tested using a vertical test stand, custom nitrous system, and data acquisition system. The computer program Chemical Equilibrium with Applications is used to compare common hybrid fuels such as sorbitol, polybutadiene acrylic acid acrylonitrile, and poly(methyl methacrylate) along with the manufactured fuel. The experimental results indicate the promise of higher performance using paraffin. The analyses, however, show that refinements in grain design are necessary to fully realize the advantages of paraffin.

Detailed thermodynamic, kinetic, geometric, and cost models are developed, implemented, and validated for the synthesis/design and operational analysis of hybrid solid oxide fuel cell (SOFC) – gas turbine (GT) – steam turbine (ST) systems ranging in size from 1.5 MWe to 10 MWe. The fuel cell model used in this thesis is based on a tubular Siemens-Westinghouse-type SOFC, which is integrated with a gas turbine and a heat recovery steam generator (HRSG) integrated in turn with a steam turbine cycle. The SOFC/GT subsystem is based on previous work done by Francesco Calise during his doctoral research (Calise, 2005). In that work, a HRSG is not used. Instead, the gas turbine exhaust is used by a number of heat exchangers to preheat the air and fuel entering the fuel cell and to provide energy for district heating. The current work considers instead the possible benefits of using the exhaust gases in an HRSG in order to produce steam which drives a steam turbine for additional power output. Four different steam turbine cycles are considered in this M.S. thesis work: a single-pressure, a dual-pressure, a triple-pressure, and a triple-pressure with reheat. The models have been developed to function both at design (full load) and off-design (partial load) conditions. In addition, different solid oxide fuel cell sizes are examined to assure a proper selection of SOFC size based on efficiency or cost. The thermoeconomic analysis includes cost functions developed specifically for the different system and component sizes (capacities) analyzed. A parametric study is used to determine the most viable system/component syntheses/designs based on maximizing total system efficiency or minimizing total system life cycle cost. / Master of Science