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Corona discharge from a RF quarter wave coaxial cavity resonator is considered as a plasma ignition source for spark ignited (SI) internal combustion (IC) engines. The gaseous discharge processes associated with this device are analyzed using principles of gas kinetics and gaseous electronics, with assumed values for the electric field strength. Corona discharge occurs when the electric field shaped and concentrated by a single electrode exceeds the breakdown potential of the surrounding gas. Ambient electrons, naturally present due to ionizing radiation, drift in the direction of the externally applied field, gaining energy while undergoing elastic collisions with neutral molecules. After gaining sufficient energy they dissociate, excite, or ionize the neutral particles through inelastic collision, creating additional electrons. This process leads to avalanche electrical breakdown of the gas within about 10-8 sec.

Crashworthiness is a measure of a vehicle's structural integrity during mechanical impact and of its ability to absorb energy and provide occupant protection in crash situations. Finite element modeling has been successfully used to simulate collision events; the present work uses these techniques to simulate the side impact of a mid-size car in order to investigate the crash characteristics of a 45 km/hr impact. Five different analyses were conducted on orthogonal and oblique impacts under varying conditions. The numerical results from the first analysis were compared with published experimental crash results, showing favorable comparisons for this numerical model prediction.

In order to prepare for flight on-board a military aircraft with an experimental prototype system, a crash scenario analysis was performed to ensure safety of the aircraft and its crew. The following describes the crash analysis of the Oculus sensor pallet system in preparation for a flight test on a C-130 aircraft. In this particular case, the two units were analyzed individually in accordance with the loading standards outlined in MIL-HDBK-1791. The unit that deploys outside of the rear cargo ramp of the aircraft (sensor platform) was analyzed more closely than the system that remains locked (operator station) into the rail system of the aircraft. As the results show, both systems are capable of being subjected to crash loading forces.