IPB. Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

Papers

1. Numerical Model for the Prediction of the Regression Rate in Hybrid Rocket Kick-Motors Working with Liquid Nitrous Oxide

2. Development of a Low-Cost Permanent Magnet Cylindrical Hall Effect Thruster for CubeSats

3. Computational Study of Plasma Detachment from Magnetic Nozzles in Applied Field MPD Thrusters using Lattice Boltzmann Method

4. Hybrid Rocket Engines as an Option to Future Application for the Brazilian Space Sector

5. high- power sounding rockets

6. Thermal Analysis of the Scramjet Engine System with Burning Fuel

8. experimental study on the influence of different oscillation amplitude on the combustion characteristics of propellant aluminum particles

9. Advantage of Using Turbopump in Hybrid Rocket Applications

11. Feasibility Study of Orbit Control Methods in CubeSats with Electric Propulsion for an Interplanetary Mission

13. investigation of parametric dynamics inside a heaterless hollow cathode (hhc)

15. research on aerodynamic drag characteristics \\of solid fuel ramjet

16. Fuel regression characteristics of axial-injection end-burning hybrid rockets using Nitrous Oxide

18. smc based heading control of a satellite model with duo cold thrusters

19. Development of a validated modular design tool for ABS-nitrous hybrid rocket engines

20. The operational range of liquid metal and ionic liquid ion sources in the pure ionic regime.

21. Interstellar space exploration using photon propulsion

22. STUDY OF EFFECT ON COMBUSTION FLOW-FIELD DUE TO VARIATION OF INLET BOUNDARY CONDITIONS IN DUAL-CAVITY SCRAMJET COMBUSTOR

23. Experiment and Simulation for Dynamic Characteristics of Dual-mode Space Propulsion System Pressurized by Electric Pump

24. Modern materials and technologies implementation into the LRE design

26. Determination of solid fuels regression rate by reactive molecular dynamics simulations

27. Novel electro-chemical miniaturized thrusters for Distributed Satellite Space Missions

28. Assessing Impurity Effects on LO-x/Methane and LO-x/Natural Gas Mixtures in Rocket Propulsion Systems

29. Atomisation and Combustion of the ONERA / CNES High Performance Green Monopropellant

30. Development and Verification of a Thrust Vector Balance for Electric Propulsion Systems

31. Challenges and Opportunities for Orbital Propulsion

32. Development of FEEP thruster based on annular-slit configured type emitter with indium propellant

33. cfd optimization of film cooling in green storable bipropellant rocket thrusters