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 |
Quentmeyer, R. J., 1977, 'Experimental Fatigue Life Investigation of Cylindrical Thrnst Chambers,' AIAA-77-893, AIAA/SAE 13th Propulsion Conference, Orlando, FL
|
10 |
Armstrong, W. H., 1981, 'Structural Analysis of Cylindrical Thrust Chambers-Final Report-Volume II, NASA CR-165241
|