Object oriented fault diagnosis system for space shuttle main engine redlines [PDF]
A great deal of attention has recently been given to Artificial Intelligence research in the area of computer aided diagnostics. Due to the dynamic and complex nature of space shuttle red-line parameters, a research effort is under way to develop a real ...
Mohapatra, Saroj Kumar, Rogers, John S.
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Fault Detection and Isolation Based on Structural Analysis: Application to a Multi-Engine Propulsion Cluster. [PDF]
Sensors (Basel)Murata R +4 more
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Atom probe tomography using an extreme ultraviolet trigger pulse. [PDF]
Rev Sci Instrum, 2023 Caplins BW +4 more
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Automatic mathematical modeling for real time simulation program (AI application) [PDF]
A methodology is described for automatic mathematical modeling and generating simulation models. The major objective was to create a user friendly environment for engineers to design, maintain, and verify their models; to automatically convert the ...
Purinton, Steve, Wang, Caroline
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A versatile sample-delivery system for X-ray photoelectron spectroscopy of in-flight aerosols and free nanoparticles at MAX IV Laboratory. [PDF]
J Synchrotron RadiatPreger C +4 more
europepmc +1 more source
Intelligent Fault Diagnosis of Liquid Rocket Engine via Interpretable LSTM with Multisensory Data. [PDF]
Sensors (Basel), 2023 Zhang X, Hua X, Zhu J, Ma M.
europepmc +1 more source
RL10A-3-3B high mixture ratio qualification program [PDF]
The results of the high mixture ratio qualification testing of the RL10 engine for the Shuttle/Centaur program are presented. The objective of the engine qualification test was to demonstrate the suitability of the RL10A-3-3B engine for space vehicle ...
Smith, C., Varella, D., Vogel, T.
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The Fate of Water in Hydrogen-Based Iron Oxide Reduction. [PDF]
Adv Sci (Weinh), 2023 El-Zoka AA +4 more
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Investigation of SSME alternate high pressure fuel turbopump lift-off seal fluid and structural dynamic interaction [PDF]
The Space Shuttle main engine (SSME) alternate turbopump development program (ATD) high pressure fuel turbopump (HPFTP) design utilizes an innovative lift-off seal (LOS) design that is located in close proximity to the turbine end bearing.
Elrod, David A.
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