Refrigerant based propulsion system for small spacecraft
Keywords and Phrases
MR SAT; R-134a refrigerant
"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.
Riggins, David W.
Mechanical and Aerospace Engineering
M.S. in Aerospace Engineering
University of Missouri--Rolla
x, 120 pages
© 2007 Carl Reiner Seubert, 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=b6065530~S5
Seubert, Carl Reiner, "Refrigerant-based propulsion system for small spacecraft" (2007). Masters Theses. 6827.