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 language | English |
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Pages (from-to) | 79-82 |
Number of pages | 4 |
Journal | Hanneng Cailiao/Chinese Journal of Energetic Materials |
Volume | 17 |
Issue number | 1 |
Publication status | Published - Feb 2009 |
Keywords
- Energy characteristics
- Furazan
- High energy propellant
- Oxidizer
- Physical chemistry
- Smokeless propellant