Space exploration is a large field that requires high performing circuitry due to the harsh environment. Within a space environment one of the biggest factors leading to circuit failure is radiation. Circuits must be robust enough to continue operation after being exposed to the high doses of radiation. Bandgap reference (BGR) circuits are designed to be voltage references that stay stable across a wide range of supply voltages and temperatures. A bandgap reference is a piece of a large circuit that supplies critical elements of the large circuit with a constant voltage. When used in a space environment with large amounts of radiation a BGR needs to maintain its output voltage to enable the rest of the circuit to operate under proper conditions. Since a BGR is not a standalone circuit it is difficult and expensive to test if a BGR is maintaining its reference voltage.

This thesis describes a methodology of isolating and simulating bandgap references. Both NPN and PNP bandgap references are simulated over a variety of radiation doses and dose rates. This methodology will allow the degradation due to radiation of a BGR to be modeled easily and affordably. It can be observed that many circuits experience enhanced low dose rate sensitivity (ELDRS) which can lead to failure at low total ionizing doses (TID) of radiation. A compact model library demonstrating degradation of transistors at both high and low dose rates (HDR and LDR) will be used to show bandgap references reliability. Specifically, two bandgap references being utilized in commercial off the shelf low dropout regulators (LDO) will be evaluated. The LDOs are reverse engineered in a simulation program with integrated circuit emphasis (SPICE). Within the two LDOs the bandgaps will be the points of interest. Of the LDOs one has a positive regulated voltage and one has a negative regulated voltage. This requires an NPN and a PNP based BGR respectively. This simulation methodology will draw conclusions about the above bandgap references, and how they operate under radiation at different doses and dose rates.

The Solar Powered Amphibious Transport (SPAT) is an amphibious hovercraft that uses solar energy as a power source and is fully controlled via iOS application on a phone or tablet. The hovercraft field is relatively unexplored with a solar power source, and one of the goals of the SPAT was to spark interest in sustainable hovercraft design. By challenging the potential of solar power, the SPAT proves that solar energy can be used in high power transportation applications. The second motive behind the creation a hovercraft was for it to serve as a disaster relief vehicle. A hovercraft can traverse both ground and water, which makes it ideal in flooded areas. With the SPAT being remote controlled it can allow the operator to stay at a safe distance while sending supplies or rescuing a person. The SPAT design covered multiple size options, however a small prototype version was built to serve as a proof of concept that a larger solar hovercraft is possible. Our analysis suggests that a larger craft will be able to carry more weight, and be more power efficient. A larger SPAT could help deliver supplies or rescue stranded people after a flood or hurricane. One issue faced however, was that many hovercrafts are highly expensive. The SPAT prototype was designed on a tight budget that did not exceed $800. The possibility of achieving this cost levels allows hovercraft to be a reasonable option for disaster relief agencies. After many long hours spent the SPAT became a fully operational remote control solar powered hovercraft.