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Title: Refrigerant-based propulsion system for small spacecraft
Alternate Title: Refrigerant based propulsion system for small spacecraft
Author (s): Seubert, Carl Reiner, 1982-
Advisor(s): Pernicka, Hank
Department/Lab Affiliations: Space Systems Engineering
Keywords: MR SAT.
R-134a refrigerant.
Issue Date: 2007
Publisher: University of Missouri-Rolla
Citation: Seubert, Carl Reiner. "Refrigerant-Based Propulsion System For Small Spacecraft." Master's Thesis, Aerospace Engineering, University of Missouri-Rolla, 2007.
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, p. iii.
Type: Thesis/Dissertation
text
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http://scholarsmine.mst.edu/thesis/Refrigerantbased_pr_09007dcc8040da15.html
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Seubert_09007dcc8040da7c.pdf



titleRefrigerant-based propulsion system for small spacecraft
title.alternativeRefrigerant based propulsion system for small spacecraft
contributor.advisorPernicka, Hank
contributor.authorSeubert, Carl Reiner, 1982-
contributor.deptlabSpace Systems Engineering
subjectMR SAT.
subjectR-134a refrigerant.
subject.LCSHRefrigerants.
subject.LCSHRockets (Aeronautics) -- Fuel.
subject.LCSHSpace vehicles -- Propulsion systems -- Design and construction.
date.issued2007
publisherUniversity of Missouri-Rolla
identifier.URI
http://scholarsmine.mst.edu/thesis/pdf/Seubert_09007dcc8040da7c.pdf
identifier.citationSeubert, Carl Reiner. "Refrigerant-Based Propulsion System For Small Spacecraft." Master's Thesis, Aerospace Engineering, University of Missouri-Rolla, 2007.
identifier.oclc124509963
descriptionIncludes bibliographical references (p. 115-119).
descriptionMode of access: World Wide Web.
descriptionSystem requirements: Adobe Acrobat Reader; Internet browser.
descriptionThe entire thesis text is included in file.
descriptionThesis (M.S.)--University of Missouri--Rolla, 2007.
descriptionTitle from title screen of thesis/dissertation PDF file (viewed May 11, 2007)
descriptionVita.
description.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, p. iii.
description.
statementOfResponsibility
by Carl Reiner Seubert.
typeThesis/Dissertation
type.DCMITypetext
rightsThese materials are protected under copyright by the original author.
language.ISO639-2eng
format.extentx, 120 p. : ill., digital, PDF file.
date.accessioned2007-12-04T14:56:28Z
date.available2007-12-17T21:13:44Z
identifier.persist.URI
http://scholarsmine.mst.edu/thesis/Refrigerantbased_pr_09007dcc8040da15.html
Full Text
Seubert_09007dcc8040da7c.pdf