DOI QR코드

DOI QR Code

Structural Analysis of Gas Generator Regenerative Cooling Chamber

재생냉각형 가스발생기 챔버 구조해석

  • Published : 2007.10.01

Abstract

Elastic-plastic structural analysis for regenerative cooling chamber of gas generator was performed. Uniaxial tension test was conducted for STS316L at room and high temperature conditions to get the material data necessary for the structural analysis of the chamber which was operated under thermal load and high internal pressure. Physical properties including thermal conductivity, specific heat and thermal expansion were also measured. The structural analysis for four different types of regenerative cooling chamber of gas generator revealed that increased cooling performance decreased the thermal load and strain of the cooling channel structure. The results propose that in order for the regenerative cooling gas generator chamber to have high structural stability with endurance to high mechanical and thermal loads, it is important for the chamber to be designed to have high cooling performance.

Keywords

References

  1. Huzel, D. K. and Huang, D. H., 1992, 'Modern Engineering for Design of Liquid-Propellant Rocket Engines,' AIAA, pp. 116-120
  2. NASA, 1972, 'Liquid Propellant Gas Generators,' NASA SP-8081
  3. Ryu, C. S., Choi, H. S. and Lee, D. J., 2005, 'Structure Design of Regenerative Cooling Chamber of Liquid Rocket Thrust Chamber,' Journal of the KSAS, Vol. 33, No. 12, pp. 109-116
  4. Standard Test Method and Definitions for Mechanical Ttesting of Steel Product, ASTM
  5. ASM International, 'ASM Metals Reference Book,' ASM International, pp. 366
  6. Armstrong, W. H. and Brogren, E. W., 1975, 'Thrust Chamber Life Prediction, Volume Il-Plug Nozzle Centerbody and Cylinder Life Analysis,' NASA-CR-200877
  7. Armstrong, W. H. and Brogren, E. W., 1976, '3-D Thrust Chamber Life Prediction,' NASA CR-134979
  8. Armstrong, W. H., 1979, 'Structural Analysis of Cylindrical Thrust Chambers-Final Report-Volume I,' NASA CR-159522
  9. Armstrong, W. H., 1981, 'Structural Analysis of Cylindrical Thrust Chambers-Final Report-Volume II, NASA CR-165241
  10. Quentmeyer, R. J., 1977, 'Experimental Fatigue Life Investigation of Cylindrical Thrnst Chambers,' AIAA-77-893, AIAA/SAE 13th Propulsion Conference, Orlando, FL

Cited by

  1. High-Temperature Deformation Behavior of a STS 321 Stainless Steel vol.20, pp.5, 2016, https://doi.org/10.6108/KSPE.2016.20.5.051