Numerical studies on specific impulse of partially filled pulse detonation rocket engines

Shigeru Sato, Akiko Matsuo, Takuma Endo, Jiro Kasahara

Research output: Contribution to journalArticle

63 Citations (Scopus)

Abstract

Performance analyses of pulse detonation rocket engines (PDREs) were numerically studied, focusing on partialfill effects at ground tests. The initial detonable mixture, inert gas, fuel-fill fraction, equivalence ratio, and initial temperature of inert gas were changed as governing parameters. The simulation results were compared against those of previous studies and agreed well with them. The simulation results indicated that the initial mass fraction of the detonable mixture to total mass of the gas was the predominant factor for the specific impulse of partially filled PDREs. Based on the numerical results, a new, simple empirical formula is proposed to predict the specific impulse of partially filled PDREs.

Original languageEnglish
Pages (from-to)64-69
Number of pages6
JournalJournal of Propulsion and Power
Volume22
Issue number1
DOIs
Publication statusPublished - 2006

ASJC Scopus subject areas

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

Fingerprint Dive into the research topics of 'Numerical studies on specific impulse of partially filled pulse detonation rocket engines'. Together they form a unique fingerprint.

  • Cite this