NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Life extending control for rocket enginesThe 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).
Document ID
19920022019
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lorenzo, C. F.
(NASA Lewis Research Center Cleveland, OH, United States)
Saus, J. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Ray, A.
(Pennsylvania State Univ. University Park., United States)
Carpino, M.
(Pennsylvania State Univ. University Park., United States)
Wu, M.-K.
(Pennsylvania State Univ. University Park., United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1992
Subject Category
Engineering (General)
Report/Patent Number
NASA-TM-105789
NAS 1.15:105789
E-7219
Report Number: NASA-TM-105789
Report Number: NAS 1.15:105789
Report Number: E-7219
Accession Number
92N31263
Funding Number(s)
PROJECT: RTOP 590-21-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available