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NASA NTRS · 20050196667

The GE-NASA RTA Hyperburner Design and Development

Abstract

The Revolutionary Turbine Accelerator (RTA) project is a ground demonstration of a Mach 4 Turbine Based Combined Cycle engine. This new combined cycle engine developed for the ground-based demonstration will use a new type of augmentor called the hyperburner. The technical features of this new augmenter are introduced in this work. Some of the salient features include a new variable area bypass injector system and a new flame holder configuration. A summary of the hyperburner configuration and the supporting evidence obtained during the hyperburner rig experiments show that hyperburner is a viable burner concept capable of meeting the goals of the RTA ground engine demonstration project.

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BibTeXRIS

Lee, Jin-Ho, Winslow, Ralph, Buehrle, Robert J.. 2005-06-01. The GE-NASA RTA Hyperburner Design and Development. https://ntrs.nasa.gov/citations/20050196667

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