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NASA NTRS · 19920022019

Life extending control for rocket engines

Abstract

The concept of life extending control is defined. A brief discussion of current fatigue life prediction methods is given and the need for an alternative life prediction model based on a continuous functional relationship is established. Two approaches to life extending control are considered: (1) the implicit approach which uses cyclic fatigue life prediction as a basis for control design; and (2) the continuous life prediction approach which requires a continuous damage law. Progress on an initial formulation of a continuous (in time) fatigue model is presented. Finally, nonlinear programming is used to develop initial results for life extension for a simplified rocket engine (model).

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BibTeXRIS

Lorenzo, C. F., Saus, J. R., Ray, A., Carpino, M., Wu, M.-K.. 1992-08-01. Life extending control for rocket engines. https://ntrs.nasa.gov/citations/19920022019

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