Effect of regenerative cooling on rocket engine specific impulse

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

研究成果: Article

8 引用 (Scopus)

抜粋

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.

元の言語English
ページ(範囲)286-288
ページ数3
ジャーナルJournal of Propulsion and Power
10
発行部数2
DOI
出版物ステータスPublished - 1994 1 1

ASJC Scopus subject areas

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

フィンガープリント Effect of regenerative cooling on rocket engine specific impulse' の研究トピックを掘り下げます。これらはともに一意のフィンガープリントを構成します。

  • これを引用

    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