NASA NTRS · 19950065354
Rocket Combustion Chambers Resist Thermal Fatigue
Abstract
Improved design concept developed for combustion chambers for rocket engines, described in three reports. Provides compliance allowing unrestrained thermal expansion in circumferential direction. Compliance lengthens life of rocket engine by reducing amount of thermal deformation caused by repeated firings.
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Kazaroff, John M., Jankovsky, Robert S., Pavli, Albert J.. 1995-04-01. Rocket Combustion Chambers Resist Thermal Fatigue. https://ntrs.nasa.gov/citations/19950065354
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