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.
Pretest uncertainty analysis for chemical rocket engine tests
1987-01-01
Conference paper
No indication
English
Pretest Analysis for Modal Survey Tests Using Fixed Base Correction Method
British Library Conference Proceedings | 2019
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