Masters Theses
Keywords and Phrases
MR SAT; R-134a refrigerant
Abstract
"The MR SAT spacecraft under development at UMR requires a propulsion system that can be utilized to perform orbital maneuvers and three-axis attitude control to complete its mission objective of conducting spacecraft formation flight. This thesis documents the research, analysis design and development of the cold gas propulsion system that was integrated on the MR SAT spacecraft"--Abstract, page iii.
Advisor(s)
Pernicka, Hank
Committee Member(s)
Riggins, David W.
Homan, Kelly
Department(s)
Mechanical and Aerospace Engineering
Degree Name
M.S. in Aerospace Engineering
Publisher
University of Missouri--Rolla
Publication Date
Spring 2007
Pagination
x, 120 pages
Rights
© 2007 Carl Reiner Seubert, All rights reserved.
Document Type
Thesis - Open Access
File Type
text
Language
English
Subject Headings
Refrigerants
Rockets (Aeronautics) -- Fuel
Space vehicles -- Propulsion systems -- Design and construction
Thesis Number
T 9162
Print OCLC #
176055357
Electronic OCLC #
124509963
Link to Catalog Record
Recommended Citation
Seubert, Carl Reiner, "Refrigerant-based propulsion system for small spacecraft" (2007). Masters Theses. 6827.
https://scholarsmine.mst.edu/masters_theses/6827
