IP. Interactive Presentations

Papers

1. GAS-CORE NUCLEAR ROCKET ENGINES AND NOT STANDARD PROPULSIVE MASS FOR THEM

2. CFD Analysis of Combustion Instability in Axial-Injected Hybrid Rocket Engines during Throttling Transient

3. Evaluation of Required Energies for Detonation of Chemical Rocket Propellants

4. Design, Study and Manufacturing of a Composite Solid Rocket Propellant

5. improvement of nonlinear coefficient on combustion instability prediction in solid rocket motors

6. Numerical modeling of large free-surface fluid flow in fuel tanks in flight

7. effect of different thermal cure cycles on the propellant curing of solid rocket motor: a numerical study

8. Investigation of wagon-wheel fuel grain design of hybrid rocket motor

9. Numerical Simulation of Inner Flow Field of a Pintle Injector Variable Thrust Hybrid Rocket Engine

10. Size effect study of grain port on a long-time working hybrid rocket motor

11. development of three variants of reverse flow multiple nozzle solid rocket motor

12. the glass-membrane MEMS igniter with improved performance for cube-sat application

13. Dr. V.A. Menshikov Association of participants of the Project "International Global Monitoring and forecasting AeroSpace System" (Association "IGMASS"), Russia.

14. Study on the Propellant Ablation Properties of Laser Ablation Propulsion

15. Numerical research on ablation of PTFE/Al propellant using continuous laser beam

16. development and qualification of a high performance solid strapon motor

17. Influence of After-burning Chamber Dome Length on Secondary Combustion for Solid Ducted Rocket Motor

18. cavity and jet injection effects on supersonic compressible ramp flow

19. The transient flow characteristics investigation of the wake behind a triangular flameholder in ramjet combustor

20. Research on the combination actuator system of adjustable nozzle in ramjet

21. 5kW Class of Annular-Geometry Ion Thruster Development

22. A Modular, Viable and Versatile System for Deployment of Solar Sail in a 3U Satellite

23. CIRA Liquid Propulsion Test Facilities: Vision and Roadmap

24. CONCEPT AND DEVELOPMENT OF USING HYDROGEN PER OXIDE AS A PROPELLEANT

25. Development of a Cryogenic Rocket Engine at Delft Aerospace Rocket Engineering

27. Development of a Next-Generation Thrust Balance with Nano-Newton Resolution

28. Development of Small Solid Rocket Boosters for the ILR-33 Sounding Rocket

29. Dynamic load identification of a second stage liquid rocket engine based on Tikhonov regularization method

30. Electric Propulsion Anomalies and Failures: Analysis of On Orbit Track Record

31. Experimental Investigation for Reliable Start-up of 5W Microwave Electrothermal Thruster as means of Primary Propulsion for Nano and Small Satellites in Realistic Space Condition

32. Experimental Investigation of Combustion in MEMS based Microthrusters

33. Experimental study on the current-sheet evolution for a pulsed inductive thruster

34. Fast Transit Access to the Outer Solar System

35. Feasibility Study on Non-catalytic Ignitor for Hydrogen Peroxide/Polyethylene Hybrid Rocket

36. Impinging Injector Design for a Paraffin-Nitrous Oxide Hybrid Rocket Engine used in Sounding Rockets Part I: CFD Simulation of Candidate Designs

37. Impinging Injector Design for a Paraffin-Nitrous Oxide Hybrid Rocket Engine used in Sounding Rockets Part II: Cold-Flow Testing of Candidate Designs

38. investigations of real-fluid characteristics in high-pressure liquid rocket engines

39. Liquid-Propellant Rocket Engines Fault Diagnostic Based on Dynamic cloud BP networks

40. Low Cost Propulsion Technique to Transfer Satellite to Low Moon Orbit

41. LV energetics increase by improvement of pneudraulic propellant feed systems characteristics of propulsion systems

42. Neuro-Fuzzy Model to Evaluate feed-back sensors of Mixture-Ratio Control System (MRCS) and control the performance of Rocket-Engine

43. Numerical Study of LOX/Kerosene Combustion in a Single Element Coaxial Bi-Swirl Injector at Supercritical Conditions

44. Progress in CIRA Development Plan on Electric Propulsion

45. System & Magnetohydrodynamic Simulation Investigation on Pulsed Inductive Thrusters

46. The kinematics analysis on sway unit of LOX/Kerosene Rocket engine

47. The LHT-100 Hall electric propulsion subsystem development for the XX-2 satellite

48. Value analysis and value-informed tradeoffs for the adoption of electric propulsion onboard communication satellites

49. Experimental Study on Combustion Characteristics of a Single Bi-Swirl Injector for Variable Thrust Lox/Kerosene Rocket Engine