rootbrowseIAC-08C4session 33. Propulsion TechnologyPapers1. Proven advanced technologies for space launcher SRM nozzles2. Influence of external factors on starting and an operation of thermal pipes as a component of the space propulsion systems3. Cryogenic Thermal Design of Electromagnetic Formation Flight Satellites4. The Development of Japanese 20N Thruster Valve for a Spacecraft Propulsion System - Qualification test result -5. feasibility study on nondestructive inspection for regenerative cooled combustion chamber by using neutron diffraction method and neutron radiography testing6. Experimental Investigation of the Evacuation Effect in Expansion Deflection Nozzles7. Space propulsion components based on GAMMA TiAl BASED ALLOYS BY COMBUSTION SYNTHESIS+COMPACTION ROUTE8. Evaluation and Characterization of Laser Ignition Conditions for RCS Thruster Using Green Propellants9. mechanical interfaces for rocket thrust chamber technology based on composite materials10. ROCKET NOZZLE DESIGN AND MANUFACTURE11. THE CALCULATION AND ANALYSIS OF FLEXIBLE JOINT ADHESION BONDED INTERFACE’S J-INTEGRAL IN SOLID ROCKET MOTOR12. Pintle-controlled solid rocket motor research13. A New Method of Model-Based Diagnosis for Spacecraft Propulsion Systems14. The DEIMOS III Engine Concept15. The improvement of the thrust and specific impulse by heating and elongating of de Laval nozzle