NASA NTRS · 19870011082
Pretest uncertainty analysis for chemical rocket engine tests
Abstract
A parametric pretest uncertainty analysis has been performed for a chemical rocket engine test at a unique 1000:1 area ratio altitude test facility. Results from the parametric study provide the error limits required in order to maintain a maximum uncertainty of 1 percent on specific impulse. Equations used in the uncertainty analysis are presented.
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Davidian, Kenneth J.. 1987-01-01. Pretest uncertainty analysis for chemical rocket engine tests. https://ntrs.nasa.gov/citations/19870011082
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