All Stories

  1. Can Reusable Heavy-lift Rockets perform Vertical Landing with an Aerospike Engine?
  2. Design Optimization of a Mg/CO2 Hybrid Rocket Engine for Mars Ascent Vehicles
  3. A Numerical Method for Burnback Analysis of UV-cured Solid Rocket Propellant Grains
  4. Numerical Investigation of Different Configurations for Hydrogen Fuelled Jet Engine Combustors
  5. Swirl Injection Modeling for Paraffin-Based Hybrid Rocket Engines Combustion Instabilities
  6. Multiphysics modelling for a hybrid rocket engine with liquefying fuel: a sensitivity analysis on combustion instability
  7. Fluidic Control of Transition in a Dual-bell Nozzle
  8. Low-order models for low-frequency combustion instability in hybrid rocket engines
  9. Preliminary study of a resonant igniter for rocket engines
  10. Acoustic Excitation as Triggering Mechanism of the “DC Shift” in Hybrid Rockets
  11. Uncertainty Analysis and Robust Design for a Hybrid Rocket Upper Stage
  12. Numerical Tool Optimization for Advanced Rocket Nozzle Performance Prediction
  13. Robust Design of Hybrid Rocket Engine for Small Satellite Launchers
  14. Plasma Actuator–Assisted Rocket Nozzle for Improved Launcher Performance
  15. Optimization of Active Debris Removal Missions with Multiple Targets
  16. Novel Comprehensive Technique for Hybrid Rocket Experimental Ballistic Data Reconstruction
  17. Pressure-Measurement Based Estimation of Fuel Regression Rate in Hybrid Rockets
  18. Modeling of Saturated and Superheated N2O Heat Transfer Rates, with Experimental Verification
  19. A Straightfotward Approach for Robust Design of Hybrid Rocket Engine Upper Stage
  20. Approximate and Exact Approaches for the Optimization of Hybrid-Rocket Upper Stage
  21. Analysis of Acoustics and Vortex Shedding Interactions in Hybrid Rocket Motors
  22. Optimization of Hybrid Upper-Stage Motor with Coupled Evolutionary/Indirect Procedure
  23. Optimization of an Advanced Open Rotor Engine for Civil Transport
  24. Optimization of Hybrid Propellant Mars Ascent Vehicle
  25. Efficient Missions to Potentially Hazardous Object 2013 TV135