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Exergy Analysis of Rocket SystemsExergy is defined as the useful work available from a system in a specified environment. Exergy analysis allows for comparison between different system designs, and allows for comparison of subsystem efficiencies within system designs. The proposed paper explores the relationship between the fundamental rocket equation and an exergy balance equation. A previously derived exergy equation related to rocket systems is investigated, and a higher fidelity analysis will be derived. The exergy assessments will enable informed, value-based decision making when comparing alternative rocket system designs, and will allow the most efficient configuration among candidate configurations to be determined.
Document ID
20150009419
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Gilbert, Andrew
(Alabama Univ. Huntsville, AL, United States)
Mesmer, Bryan
(Alabama Univ. Huntsville, AL, United States)
Watson, Michael D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
June 3, 2015
Publication Date
April 13, 2015
Subject Category
Engineering (General)
Launch Vehicles And Launch Operations
Report/Patent Number
M15-4472
Report Number: M15-4472
Meeting Information
Meeting: IEEE Systems Conference
Location: Vancouver, BC
Country: Canada
Start Date: April 13, 2015
End Date: April 16, 2015
Sponsors: Institute of Electrical and Electronics Engineers
Distribution Limits
Public
Copyright
Public Use Permitted.
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