Abstract
The energy parameters of the propellant containing octanitrocubane (ONC) are calculated by CAD system of propellant energy calculation under standard condition (pc/po=70:1). Replacing ammonium perchlorate with octanitrocubane in HTPB propellant increases the specific impulse for 125 N·s·kg-1, NC/NG/ONC smokeless MDB propellant has a specific impulse of 2545 N·s·kg-1, GAP/ONC/RDX smokeless propellant has a high specific impulse over 2600 N·s·kg-1 in very wide scope.
| Original language | English |
|---|---|
| Pages (from-to) | 367-369 |
| Number of pages | 3 |
| Journal | Hanneng Cailiao/Chinese Journal of Energetic Materials |
| Volume | 15 |
| Issue number | 4 |
| Publication status | Published - Aug 2007 |
Keywords
- Energy characteristics
- High energy propellant
- Otanitrocubane
- Oxidizer
- Physical chemistry
- Smokeless propellant