4.5 Article

Localized characteristic velocity (c*) for rocket combustion analysis based on gas temperature and composition via laser absorption spectroscopy

期刊

MEASUREMENT SCIENCE AND TECHNOLOGY
卷 32, 期 12, 页码 -

出版社

IOP Publishing Ltd
DOI: 10.1088/1361-6501/ac18d3

关键词

characteristic velocity; hybrid rockets; liquid-propellant rockets; absorption spectroscopy; rocket combustion

资金

  1. Air Force Research Laboratory [16-EPA-RQ-09]
  2. NASA Jet Propulsion Laboratory [1616608]
  3. Eugene V. Cota-Robles Fellowship
  4. 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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