Now showing items 1-2 of 2
Propulsion Subsystem Thermal Modeling for the FalconSat-5 Microspacecraft
A high fidelity thermal model was developed to insure that propulsion and payload thermal requirements are maintained during FalconSat-5's useful life and flight operations. The unique propulsion subsystem on-board the ...
On-Demand Droplet Generation
Contributor:Laabs, Shawn; Cornella, Barry Michael; Hammerland, Sean Sawyer
The objective of this design project was to develop a working on demand droplet generator for use in ambient conditions as well as in a vacuum environment. The primary design parameters set by this project include the ...