Burning rate of polyurethane composite propellant with energetic nano-composite additives | ||||
| International Conference on Aerospace Sciences and Aviation Technology | ||||
| Article 3, Volume 18, Issue 18, April 2019, Page 1-8 PDF (737.69 K) | ||||
| Document Type: Original Article | ||||
| DOI: 10.1088/1757-899X/610/1/012001 | ||||
 View on SCiNiTO | ||||
| Authors | ||||
| Sayed Tawfik1; Ahmed Saleh1; Ahmed Elbeih2 | ||||
| 1Science and Technology Center of Excellence (STCE), El- Salam City, Cairo, Egypt. | ||||
| 2Military Technical College, Kobry Elkobbah, Cairo, Egypt. | ||||
| Abstract | ||||
| In this study, some improvements in the burning rate of hydroxyl-terminated polybutadiene (HTPB) based composite propellant was performed by introducing innovative fast burning energetic Al-Cu nanocomposite s (ACNs). By comparison with the reference composite propellant (based on nano-Al), the results showed the effectiveness of ACNs to improve the characteristics of HTPB composite propellant. The concentration effect of ANCs on the characteristics of HTPB propellant and the possibility of achieving further performance enhancement were studied. The main results have indicated that ACNs based propellants have achieved improvements in the combustion heat, burning rate, ignitability, and mechanical properties. | ||||
| Keywords | ||||
| composite propellant; Al-Cu nanocomposites; combustion heat; burning rate | ||||
|
Statistics Article View: 104 PDF Download: 135 |
||||
