Theses/Project Reports from 2018
A Carrier-Pigeon UAS for South Pole Data Transfer, Shaun P. Wixted
Orbital Optimization of Interplanetary Trajectories with Environmental Perturbations, Eric S. Woods
Theses/Project Reports from 2017
Alternative Mission Concepts for the Exploration of Outer Planets Using Small Satellite Swarms, Andrew Gene Blocher
Whitespace Exploration, Jason Lloyd Daniel
Atomic Oxygen Considerations for LEO De-orbit Trajectories Using Solar Sails, Daniel A. Fugett
Refurbished and 3D Modeled Thermal Vacuum Chamber, Lauren M. Glenn
Effects of Atomic Oxygen on the Vacuum-Induced Mass Loss Properties of a Variety of Spacecraft Materials, Tyler Harty
A Comparison Study of Composite Laminated Plates with Holes Under Tension, Joun S. Kim
Optimum Design of Composite Wing Spar Subjected to Fatigue Loadings, Juan Reuben Lazarin
Modeling and Simulation of a Sounding Rocket Active Stabilization System, Steven M. Maclean
An Investigation of Avian Wing Tip Vortex Generation Using a Biomimetic Approach, David Stewart Martin
Wing Deflection Analysis of 3D Printed Wind Tunnel Models, Matthew G. Paul
The Collisional Evolution of Orbital Debris in Geopotential Wells and Disposal Orbits, Benjamin Polzine
Mass Estimation Through Fusion of Astrometric and Photometric Data Collection with Application to High Area-to-Mass Ratio Objects, Matthew Richardson
Manufacturing and Instrumentation of an Open End Compressed Air Shock Tube, Josue O. Ruiz
Spacecraft Trajectory Optimization Suite (STOPS): Optimization of Low-Thrust Interplanetary Spacecraft Trajectories Using Modern Optimization Techniques, Shane P. Sheehan
Orbital Determination Feasibility of LEO Nanosatellites Using Small Aperture Telescopes, Michael R. Strange
The Effect of Biocomposite Material in a Composite Structure Under Compression Loading, Benjamin Andrew Sweeney
Theses/Project Reports from 2016
Effects of Curing Cycle and Loading Rates on the Bearing Stress of Double Shear Composite Joints, Mateja Andrejic
Risk-Based Approach to Assessment of Advanced Technologies for Conceptual Design, Adipratnia Asmady
Assessment of Asymmetric Flight on Solar UAS, Eric Belfield
Effect of Low Velocity Impact on the Vibrational Behavior of a Composite Wing, Richard M. De Luna
Design, Manufacture, Dynamic Testing, and Finite Element Analysis of a Composite 6u Cubesat, Yanina Soledad Hallak
A Solution to the Circular Restricted N Body Problem in Planetary Systems, Jay R. Iuliano
Subsystem Failure Analysis Within the Horizon Simulation Framework, Ian M. Lunsford