This project seeks to relate chemical composition of hop oil extracts to their measured sensory qualities. Sensory properties of beer are the result of their unique chemical makeup fingerprint. Feature selection implemented in this analysis allows subtle differences in composition to be related to sensory profiles. Separation and content identification of the extracts was achieved with gas chromatography – mass spectrometry (GC-MS) instrumentation. Data pre-processing and analysis were completed using MATLAB software and peak finding algorithms developed exclusively by in-lab personnel. Feature selection strategies facilitated the comparison of individual analyte peak heights to sensory data. Several selection methodologies were tested to compare their utility in finding correlations. These approaches included data tiling and peak table-based strategies. The mathematical nature of data correlation, linear or otherwise, was then investigated. Preliminary results suggest that there may be a complex relationship between the sensory profiles and chemical composition. Exploration in this research path will enable the use of data analysis methods developed herein to better determine which compounds present in food and drink contribute to unique sensory attributes.

Hosted through the Earth and Space Sciences department, HuskySat-1 is a 3U (30cm x 10cm x 10cm) satellite manifested for launch into low earth orbit in late 2018 or early 2019. HuskySat-1 is primarily an undergraduate research effort, but includes graduate students and industry partnerships. It spans many departments including Earth and Space Sciences, Electrical Engineering, Mechanical Engineering, Aerospace Engineering, Physics, Mathematics, and many others. The mission goals are to establish a space presence for the University of Washington, and to test novel hardware fabricated here at the University of Washington. Of particular interest are the Pulsed Plasma Thruster (PPT), a plasma propulsion device designed and fabricated entirely at the University of Washington in the Advanced Propulsion Labratory, and the K-band communication system, a high-frequency, high-gain antenna capable of transmitting data at megabits per second from orbit to Earth. The satellite also includes several other subsystems including power, attitude control, structures, computers and data handling, and low-gain communication. The mission strives to provide experience in real-life engineering to the entire team, and we achieve this by attempting to build as much of each of these subsystems from scratch as possible. Not only does this provide the most possible experience, but we are also able to grow our mission scope and customize our requirements without the excessive budget attached with many pre-made satellite components. We plan to present on the current and planned state of the mission, what we have learned in the process of designing and building this mission, and our next plans for further space exploration at the University of Washington.

This project aims to ground truth a statistical model created previously by our lab. The model predicts the characteristics of a hyper velocity impact of a projectile into both sea ice and water ice. We compared the modeling program’s simulated results with observed results from both 1.5 inch and 4 inch ice perpetrators on lab created water ice and naturally forming sea ice respectively and studying such characteristics such as peak ejection angle, maximum crater depth, and crater diameter. The experimental results are compared with the simulation presented by Koch 2017. We will apply both our experimental data and our simulation data in the design and creation of a two-stage penetration probe. The first stage is a hyper-velocity penetrator. The second stage is an aero-breaking probe that will use the plume created by the first stage to reduce its velocity before impacting the surface.