Effect of regenerative cooling on rocket engine specific impulse

Takeshi Kanda, Goro Masuya, Yoshio Wakamatsu, Akio Kanirui, Nobuo Chnizei, Masayuki Niino

Research output: Contribution to journalArticle

8 Citations (Scopus)

Abstract

In this Note, to investigate the effect of regenerative cooling on rocket engine specific impulse, whole liquid rocket engine was studied with quasi-one-dimensional simulation, taking the entropy increment of coolant into consideration.

Original languageEnglish
Pages (from-to)286-288
Number of pages3
JournalJournal of Propulsion and Power
Volume10
Issue number2
DOIs
Publication statusPublished - 1994 Jan 1

ASJC Scopus subject areas

  • Aerospace Engineering
  • Fuel Technology
  • Mechanical Engineering
  • Space and Planetary Science

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    Kanda, T., Masuya, G., Wakamatsu, Y., Kanirui, A., Chnizei, N., & Niino, M. (1994). Effect of regenerative cooling on rocket engine specific impulse. Journal of Propulsion and Power, 10(2), 286-288. https://doi.org/10.2514/3.23741