Graduation Semester and Year
2013
Language
English
Document Type
Thesis
Degree Name
Master of Science in Aerospace Engineering
Department
Mechanical and Aerospace Engineering
First Advisor
Ben Harris
Abstract
The scope of this research is the design and development of a self-stabilizing re-entry vehicle that closely resembles naturally occurring seeds in nature. It was hypothesized that a femto-satellite with a shape of a samara could self stabilize and passively generate lift, as well as transmit a signal during its descent through the atmosphere. The research included a conceptual design phase and a preliminary design phase that entailed analytic simulations, and an experimental demonstration. The goal was to investigate the feasibility of developing the above-mentioned femto-vehicle that could increase the range capability of its descent to maximize data capture.
Disciplines
Aerospace Engineering | Engineering | Mechanical Engineering
License
This work is licensed under a Creative Commons Attribution-NonCommercial-Share Alike 4.0 International License.
Recommended Citation
Lalloobhai, Amit Desai, "The Samara Spacecraft: Design And Development Of A Self-stabilizing, Auto-rotating, Distributed Sensing System" (2013). Mechanical and Aerospace Engineering Theses. 164.
https://mavmatrix.uta.edu/mechaerospace_theses/164
Comments
Degree granted by The University of Texas at Arlington