Journal
MEASUREMENT SCIENCE AND TECHNOLOGY
Volume 32, Issue 12, Pages -Publisher
IOP Publishing Ltd
DOI: 10.1088/1361-6501/ac18d3
Keywords
characteristic velocity; hybrid rockets; liquid-propellant rockets; absorption spectroscopy; rocket combustion
Funding
- Air Force Research Laboratory [16-EPA-RQ-09]
- NASA Jet Propulsion Laboratory [1616608]
- Eugene V. Cota-Robles Fellowship
- Natural Sciences and Engineering Research Council of Canada (NSERC)
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The method proposed in this work allows for experimentally determining a local characteristic velocity c*, providing reliable data support for further research.
In this work, a method for experimentally determining a local characteristic velocity, c*
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