| 1 |
Application of 3D energetic metal-organic frameworks containing Cu as the combustion catalyst to composite solid propellant
Liu YF, Jin SH, Yang HT, Li SH, Xie WX, Zhao Y, Zhang W, Chen Y, Fan XZ
Combustion and Flame, 225, 57, 2021 |
| 2 |
Characterization of Aluminum Powders: IV. Effect of Nanometals on the Combustion of Aluminized Ammonium Nitrate-Based Solid Propellants
Gromov AA, Popenko EM, Sergienko AV, Slyusarsky KV, Nalivaiko AY, Ozherelkov DY, Larionov KB, Dzidziguri EL
Propellants Explosives Pyrotechnics, 46(3), 450, 2021 |
| 3 |
Characterization of Aluminum Powders: IV. Effect of Nanometals on the Combustion of Aluminized Ammonium Nitrate-Based Solid Propellants
Gromov AA, Popenko EM, Sergienko AV, Slyusarsky KV, Nalivaiko AY, Ozherelkov DY, Larionov KB, Dzidziguri EL
Propellants Explosives Pyrotechnics, 46(3), 450, 2021 |
| 4 |
Thermo-physical Properties and Combustion Wave Aspects of RDX Contain Low Aluminium Composite Propellant
Kalal RK, Jangid SK, Shekhar H, Alegaonkar PS, Kumar A
Combustion and Flame, 218, 12, 2020 |
| 5 |
Control the combustion behavior of solid propellants by using core-shell Al-based composites
He W, Lyu JY, Tang DY, He GQ, Liu PJ, Yan QL
Combustion and Flame, 221, 441, 2020 |
| 6 |
A Promising Fuel for Variable Thrust Motor: HTPB Propellant with High Pressure Exponent
Ma S, Xu HX, Shi XB, Li Y, Li YH, Zeng LY, Fan HJ, Ran XL
Propellants Explosives Pyrotechnics, 45(9), 1366, 2020 |
| 7 |
A Promising Fuel for Variable Thrust Motor: HTPB Propellant with High Pressure Exponent
Ma S, Xu HX, Shi XB, Li Y, Li YH, Zeng LY, Fan HJ, Ran XL
Propellants Explosives Pyrotechnics, 45(9), 1366, 2020 |
| 8 |
Combustion characteristics of solid propellants under high-temperature dense-particle erosion conditions
Li J, Ma K, Lv X, Liu PJ, He GQ, Liu Y, Chen J
Combustion and Flame, 204, 49, 2019 |
| 9 |
Combustion wave of metalized extruded double-base propellants
Elbasuney S, Fahd A
Fuel, 237, 1274, 2019 |
| 10 |
Experimental Investigation of Characteristic Length Influence on a Combustion Chamber Performance with Liquid and Gelled UDMH/IRFNA Bi-propellants
Moghaddam AS, Rezaei MR, Tavangar S
Propellants Explosives Pyrotechnics, 44(9), 1154, 2019 |
