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
16 pages
Report
No indication
English
Pretest Analysis for Modal Survey Tests Using Fixed Base Correction Method
British Library Conference Proceedings | 2019
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