Energy characteristics computation of propellant containing 3,3'-dinitro-4,4'-oxazafurazan

Xu Peng Wang*, Yun Jun Luo, Kai Guo, Yong Lv

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

9 Citations (Scopus)

Abstract

The energy parameters of the propellant containing 3,3'-dinitro-4,4'-oxazafurazan (DNOAF) were calculated under standard condition(pc/po=70:1). Replacing ammonium perchlorate(AP) with DNOAF in HTPB propellant increases the specific impulse for 120 N · s · kg-1, and NC/NG/DNOAF smokeless CMDB propellant has a specific impulse of 2558 N · s · kg-1, and replacing HMX with DNOAF in PET/NG/DEGDN/HMX propellant increases the specific impulse for 194 N · s · kg-1.

Original languageEnglish
Pages (from-to)79-82
Number of pages4
JournalHanneng Cailiao/Chinese Journal of Energetic Materials
Volume17
Issue number1
Publication statusPublished - Feb 2009

Keywords

  • Energy characteristics
  • Furazan
  • High energy propellant
  • Oxidizer
  • Physical chemistry
  • Smokeless propellant

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