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Combustion Experiment to Evaluate a LOX Vaporization Nozzle for a Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine with a 1500N-Thrust

  • KITAGAWA K
  • SAKURAZAWA T
  • YUASA S
SPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES (2007) 6 47-54
DOI: 10.2322/stj.6.47
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KITAGAWA, K., SAKURAZAWA, T., & YUASA, S. (2007). Combustion Experiment to Evaluate a LOX Vaporization Nozzle for a Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine with a 1500N-Thrust. SPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 6, 47–54. https://doi.org/10.2322/stj.6.47

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