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  • IAC-08
  • C4
  • session 3
  • 3. Propulsion Technology

    Papers

    1. Proven advanced technologies for space launcher SRM nozzles

    2. Influence of external factors on starting and an operation of thermal pipes as a component of the space propulsion systems

    3. Cryogenic Thermal Design of Electromagnetic Formation Flight Satellites

    4. 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 testing

    6. Experimental Investigation of the Evacuation Effect in Expansion Deflection Nozzles

    7. Space propulsion components based on GAMMA TiAl BASED ALLOYS BY COMBUSTION SYNTHESIS+COMPACTION ROUTE

    8. Evaluation and Characterization of Laser Ignition Conditions for RCS Thruster Using Green Propellants

    9. mechanical interfaces for rocket thrust chamber technology based on composite materials

    10. ROCKET NOZZLE DESIGN AND MANUFACTURE

    11. THE CALCULATION AND ANALYSIS OF FLEXIBLE JOINT ADHESION BONDED INTERFACE’S J-INTEGRAL IN SOLID ROCKET MOTOR

    12. Pintle-controlled solid rocket motor research

    13. A New Method of Model-Based Diagnosis for Spacecraft Propulsion Systems

    14. The DEIMOS III Engine Concept

    15. The improvement of the thrust and specific impulse by heating and elongating of de Laval nozzle