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Overview of Engineering Design and Analysis at the NASA John C. Stennis Space Center

By Harry Ryan, Richard Kirkpatrick, Jared Congiardo and Justin Junell

Abstract

A wide range of rocket propulsion test work occurs at the NASA John C. Stennis Space Center (SSC) including full-scale engine test activities at test facilities A-1, A-2, B-1 and B-2 as well as combustion device research and development activities at the E-Complex (E-1, E-2, E-3 and E-4) test facilities. The propulsion test engineer at NASA SSC faces many challenges associated with designing and operating a test facility due to the extreme operating conditions (e.g., cryogenic temperatures, high pressures) of the various system components and the uniqueness of many of the components and systems. The purpose of this paper is to briefly describe the NASA SSC Engineering Science Directorate s design and analysis processes, experience, and modeling techniques that are used to design and support the operation of unique rocket propulsion test facilities

Topics: Aircraft Propulsion and Power
Year: 2007
OAI identifier: oai:casi.ntrs.nasa.gov:20070004888
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