Keywords and Phrases
"The Missouri Science and Technology Satellite (M-SAT) design team on the campus of the Missouri University of Science and Technology has developed a pair of satellites to perform an autonomous formation flight mission. To enable the mission, a unique cold gas propulsion system was developed which utilizes the refrigerant R-134a as propellant. This thesis details the design process and considerations which led to the propulsion system as integrated into the satellite for the Flight Competition Review of the NS4 competition. The design process described flowed from the mission requirements and program restrictions down through component-level requirements and resulted in a system capable of performing the assigned duties. The hazard analysis conducted for this thesis also expanded on previous analyses to address key issues and AFRL concerns"--Abstract, page iii.
Riggins, David W.
Isaac, Kakkattukuzhy M.
Mechanical and Aerospace Engineering
M.S. in Aerospace Engineering
Missouri University of Science and Technology
xiii, 204 pages
© 2009 Joseph R. Siebert, All rights reserved.
Thesis - Open Access
Library of Congress Subject Headings
Rockets (Aeronautics) -- Fuel
Space vehicles -- Propulsion systems -- Design and construction
Print OCLC #
Electronic OCLC #
Link to Catalog Recordhttp://laurel.lso.missouri.edu/record=b7076924~S5
Siebert, Joseph R., "Design hazard analysis, and system level testing of a university propulsion system for spacecraft application" (2009). Masters Theses. 4656.