Abstract
The present work is to computationally analyze side loads in a thrust-optimized parabolic nozzle during high-altitude testing. The engine startup and shutdown processes of the Korean Space Launch V...
Funding Information
  • National Research Foundation of Korea (NRF-2017M1A3A1A02014265)
  • Korea Institute of Science and Technology Information (KSC-2018-CRE-0061, K-20-L02-C05-S01)

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