4. Solid and Hybrid Propulsion (2)

Papers

1. A Novel Coordinated Energetic Compound Leading a Promising Concept of Propellant Formula Designing

2. Energetic hybrid rocket propellants for upper stage propulsion

3. Performance evaluation of modified loose flap venting scheme introduced for the propellant processing of upper stage SRM through hot test

4. Experimental Parametric Study of Rocket Grain Configuration on Potassium Nitrate Propellant with Additives employing Rocket Motor Design Computational Fluid Dynamics

5. Development of a Thrust Control System for Rocket Engines

6. Experimental and Numerical Study on Feasibility of 5kN Thrust Level Hybrid Rocket Motor using the Low-Melting-Point Thermoplastic Fuel

7. numerical and experimental research on ablation performance of a carbon/carbon composties solid rocket motor nozzle insert

8. Experimental investigation on the anti-ablation properties of multi-material interface nozzle insert in hybrid rocket motors

11. Study on thermoacoustic oscillation characteristics of carbon nanotubes

13. Experimental investigation of a flow-oriented throttleable injector designed for throttleable hybrid rocket motor

15. Using Lagrangian Coherent Structures to investigate flow field of the hot stage separation of a multistage rocket