Refrigerant-based propulsion system for small spacecraft

Author

Carl Reiner Seubert

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

RefrigerantsRockets (Aeronautics) -- FuelSpace vehicles -- Propulsion systems -- Design and construction

Thesis Number

T 9162

Print OCLC #

176055357

Electronic OCLC #

124509963

Recommended Citation

Seubert, Carl Reiner, "Refrigerant-based propulsion system for small spacecraft" (2007). Masters Theses. 6827.
https://scholarsmine.mst.edu/masters_theses/6827