참고문헌 (13)

1. Twichell, S.E. and R.B. Keller Jr., "Solid？Rocket Motor Internal Insulation," NASA？SP-8093, 1976. 

2. Natali, Maurizio, Jose Maria Kenny and？Luigi Torre, "Science and Technology of？Polymeric Ablative Materials for Thermal？Protection Systems and Propulsion Devices:？A review," Prog. Mater. Sci., Vol. 84, pp.？192-275, 2016. 

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3. Rindal, R., Flood, D. and Kendall, R.,？"Analytical and Experimental Study of？Ablation Material for Rocket Engine？Application," NASA CR-54757, 15, 1966. 

4. Bae, J.Y., Kim, T.H., Kim, J.H., Ham, H.C.？and Cho, H.H., "Conjugate Simulation of？Heat Transfer and Ablation in a Small？Rocket Nozzle," J. Comput. Struct. Eng.,？Vol. 30, No. 2, pp. 119-125, 2017. 

5. Brewer, William D., "Graphite and？Ablative Material Response to CO 2 -Laser,？Carbon-Arc, and Xenon-Arc Radiation,"？NASA, Washington, D.C., 1976. 

6. Koo, J., Lin, S., Kneer, M. and Miller, M.,？"Comparison of Ablative Materials in a？Simulated Solid Rocket Exhaust Environment,"？AIAA 32nd Structures, Structural Dynamics,？and Materials Conference, Baltimore, MD,？U.S.A., p. 978, 1991. 

7. Russell, Gerald W. and Forrest Strobel,？"Modeling Approach for Intumescing？Charring Heatshield Materials," Journal of？Spacecraft and Rockets, Vol. 43, No. 4, pp.？739-749, 2006. 

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8. Jiang Li, Kun Xi, Xiang Lv, Qiang Li and？Shu-xian Wang, "Characteristics and？Formation Mechanism of Compact/Porous？Structures in Char Layers of EPDM？Insulation Materials," Carbon, Vol. 127, pp.？498-509, 2018. 

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9. Kang, Y.G. and Park, J.H., "A Comparison？with Thermal Reaction Characteristic of？Kevlar/EPDM Internal Insulator by Change？of Chamber Pressure," Journal of the Korean？Society of Propulsion Engineers, Vol. 20, No.？3, pp. 71-77, 2016. 

10. Boyarintsev, V.I. and Zvyagin, Y., "The？Ablation of Graphite in the Turbulent Flow？of a Reacting Gas," WRIGHT-PATTERSON？AFB OHIO No. FTD-MT-24-1754-71, 1972. 

11. Blaine E. Pearce, "Radiative Heat Transfer？within a Solid-Propellant Rocket Motor,"？Journal of Spacecraft and Rockets, Vol. 15,？No. 2, pp. 125-128, 1978. 

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12. D.R. Bartz, "Turbulent Boundary-Lyer Heat？Transfer from Rapidly Accelerating Flow of？Rocket Combustion Gases and of Heated？Air," Jet Propulsion Laboratory Tech. Rep.？NASA-CR-62615, California, 1963. 

13. McBride, Bonnie J., "Computer Program？for Calculation of Complex Chemical？Equilibrium Compositions and Applications,"？NASA Lewis Research Center, 1996.