Spacecraft
Propulsion System Project – Professor James Cutler
The
purpose of this project was to design a propulsion system to transport a small
satellite from Earth’s orbit to the orbit of the Mars moon Phobos. This involved
conducting a trade study to determine what kind of propulsion system (e.g.
electrical, chemical) to use, using criteria such as system and propellant
mass, maximum and minimum thrust, and required power. Once a system was decided
upon, another trade study was conducted to determine what type of fuel and
oxidizer to use, using criteria such as ease of ignition and specific impulse.
Next, we did some research to determine the appropriate nozzle, tanks, and
valves for the system. Various calculations were performed to determine the
volume of the tanks and ratio and volume of the fuel and oxidizer. MATLAB
simulations were performed to determine the orbit this system would create and
whether it would be sufficient enough to reach the desired orbit. All of this
project, including the final report and presentation portion, was conducted via
computer in the aerospace engineering building’s computer lab. This project
taught me how to use trade studies in making design decisions, how to simulate
orbits and trajectories in MATLAB, and how to use calculations to set design
parameters.
Exhaust-Driven
Fan Testing – Professor Tim Smith/Professor Donald Geister
The
purpose of this project was to develop a design process for an exhaust-driven
fan for use by a student team. The goals of the fan were to maximize its thrust
to weight ratio while minimizing its thrust specific fuel consumption. Using an
already-developed thrust stand in the aerospace lab, we tested three different
propellers for thrust, velocity, and power output. After calibrating the thrust
stand, we took the pertinent measurements and used them to calculate the thrust
to weight ratio and thrust specific fuel consumption. From these numbers, we
could recommend a design for the student team to use. This project taught me
how to properly conduct tests using a thrust stand and how to interpret the
data it creates. It also taught me how to compile and present lab data in a
digestible and understandable manner and gave me an idea of the parameters that
go into the design of fan blades.
Cubesat
Re-entry Project – Professor James Cutler
The
purpose of this project was to develop a structure to help a Cubesat satellite
safely re-enter Earth’s orbit after collecting data. This project involved
researching current technology that was feasible for this mission and working
it down to a smaller scale to fit the requirements. We designed an Inflatable
Aerodynamic Decelerator to protect the scientific payload. Using MATLAB, orbit simulations
for the re-entry were performed and a landing zone for the spacecraft was
determined. We also used MATLAB to map the performance of the IAD. Power and
communication systems were researched and from this data, we calculated the
power needed to operate the system. This project taught me how to use already
existing technology and apply it to a smaller scale. I learned how to research
and compare different power and communication hardware and find products that
would fit within our power requirements.
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