11. Low-Power Water-Vapor Generation using Ultrasonic Atomizer for Use with Microwave Electrothermal Thrusters Open Access Author: Detwiler, Jonathan Title: Low-Power Water-Vapor Generation using Ultrasonic Atomizer for Use with Microwave Electrothermal Thrusters Area of Honors: Aerospace Engineering Keywords: METElectric PropulsionAtomizerUltrasonicMicrowaveWater VaporAerospacePropulsion File: Download Jonathan_Detwiler_Thesis_Final.pdf Thesis Supervisors: Sven G Bilen, Thesis SupervisorRobert G. Melton, Thesis Honors Advisor
12. Design of a rotor test stand for use in a compressed test facility Open Access Author: Gudall, Casey Title: Design of a rotor test stand for use in a compressed test facility Area of Honors: Aerospace Engineering Keywords: AerospaceVLRCOERotorcraft File: Download Schreyer_Honors_Thesis_Final.pdf Thesis Supervisors: Mark A Miller, Thesis SupervisorKenneth Steven Brentner, Thesis Honors Advisor
13. Evaluating Aerodynamic Performance of Coaxial Rotor Separation Distance Open Access Author: Funkhouser, Aden Title: Evaluating Aerodynamic Performance of Coaxial Rotor Separation Distance Area of Honors: Aerospace Engineering Keywords: AerospaceCoaxial RotorsThrustTorqueEngineering File: Download Evaluating_Aerodyanmic_Performance_of_Coaxial_Rotor_Separation_Distance_Final_Submission_Document.pdf Thesis Supervisors: Jose Palacios, Thesis SupervisorNamiko Yamamoto, Thesis Honors Advisor
14. Collision Avoidance of Dynamic Obstacles Utilizing a Potential Flow Theory Approach Open Access Author: Pence, Jack Title: Collision Avoidance of Dynamic Obstacles Utilizing a Potential Flow Theory Approach Area of Honors: Aerospace Engineering Keywords: Aerospacecollision avoidanceflight testautonomyautonomous flightcontrols and dynamicsnavigationcontrolsimulationguidancedroneuavuam File: Download COLLISION_AVOIDANCE_OF_DYNAMIC_OBSTACLES_UTILIZING_A_POTENTIAL_FLOW.pdf Thesis Supervisors: Jacob Willem Langelaan, Thesis SupervisorSven Schmitz, Thesis Honors Advisor
15. Accurate State Uncertainty Propagation for a Spacecraft in the Cislunar Regime Open Access Author: Glenn, Andrew Title: Accurate State Uncertainty Propagation for a Spacecraft in the Cislunar Regime Area of Honors: Aerospace Engineering Keywords: AerospaceCislunarCircular Restricted Three Body ProblemConjugate Unscented Transform File: Download Glenn_Andrew_Thesis.pdf Thesis Supervisors: Puneet Singla, Thesis SupervisorRobert G. Melton, Thesis Honors Advisor
