참고문헌 (19)

1. NASA, "Solid Propellant Grain Design and Internal Ballistics," NASA SP 8076, 1972. 

2. Sung, H.G., Kim, J.R., Choi, Y.G. and Hwang, K., "A Study on Single Chamber Dual Thrust Solid Rocket Motor," KSAS 1989 Spring Conference, Korea, pp. 163-166, April 1989. 

3. El-Nady, A.M., Ahmed, M.Y.M., El-Senbawy, M.A. and Sarhan, A.M., "Experimental and Theoretical Study on a Dual-thrust Rocket Motor with Subsonic Intermediate Nozzle," Journal of Aerospace Engineering, Vol. 232, No. 10, pp. 1844- 1852, 2018. 

4. Kim, H. and Moon, K., "Internal Ballistic Analysis using Two Kinds of Propellant for Design of Dual-thrust Solid Rocket Motor," 2017 KSPE Spring Conference, Jeju, Korea, pp. 1176-1179, May 2017. 

5. Gawad, A.R.A., Ahmed, M.Y.M., Abdalla, H.M. and El-Senbawy, M.A., "Pressure Profile Prediction of Dual-thrust Rocket Motors under Uncertainties," Propellants, Explosives, Pyrotechnics, Vol. 41, pp. 965-971, 2016. 

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6. Lee, D.H., "A Study on the Performance Prediction Technique of the Dual-thrust Rocket Motor," Journal of the Korean Society of Propulsion Engineers, Vol. 5, No. 2, pp. 38-43, 2001. 

7. Raza, M.A. and Liang, W., "Design and Optimization of 3D Wagon Wheel Grain for Dual Thrust Solid Rocket Motors," Propellants, Explosives, Pyrotechnics, Vol. 38, pp. 67-74, 2013. 

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8. Raza, M.A. and Liang, W., "Robust Design Optimization of Dual Thrust Solid Propellant Motors due to Burning Rate Uncertainties," Propellants, Explosives, Pyrotechnics, Vol. 37, pp. 476-488, 2012. 

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9. Kurva, R., Ukey, S., Modgi, M. and Mehilal, "Experimental Approaches to Develop a High Thrust Ratio in a Single Chamber Dual Thrust Motor Using a Composite Propellant Formulation based on HTPB/AP/Al," Central European Journal of Energetic Materials, Vol. 14, No. 4, pp. 917-932, 2017. 

   

10. Kumar, V.R.S., Raghunandan, B.N., Kawakami, T., Kim, H.D., Setoguchi, T. and Raghunathan, S., "Boundary-layer Effects on Internal Flow Choking in Dual-thrust Solid Rocket Motors," Journal of Propulsion and Power, Vol. 24, No. 2, pp. 224-235, 2008. 

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11. Lee, D.H., Yoon, M.W. and Hwang, K., "Development of the Dual-thrust Rocket Motor," Journal of the Korean Society of Aeronautical and Space Sciences, Vol. 32, No. 9, pp. 130-135, 2004. 

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12. Sung, H.G., Byun, J.R. and Kim, Y.G., "A Study on the Determination of the Performance Correction Factors of Solid Rocket Motors," Journal of the Korean Society of Propulsion Engineers, Vol. 5, No. 4, pp. 57-66, 2001. 

13. Sutton, G.P. and Biblarz, O., Rocket Propulsion Elements, 9th ed., John Wiley & Sons, Inc., Hoboken, N.J., U.S.A., Ch. 3, 2017. 

14. Fry, R.S., "Solid Propellant Test Motor Scaling," CPTR 73, 2001. 

15. NASA, "Solid Rocket Motor Performance Analysis and Prediction," NASA SP 8039, 1971. 

16. Gordon, S. and McBride, B.J., "Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications: I. Analysis," NASA RP 1311, 1994. 

17. Gordon, S. and McBride, B.J., "Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications: II. User Manual and Program Description," NASA RP 1311, 1996. 

18. Jung, S., Won, J., Choi, Y., Hwang, H. and Yoo, K., "Review of Solid Propellant Continuous Mix Process," 2007 KSPE Spring Conference, Seoul, Korea, pp. 197-200, April 2007. 

19. Fang, S., Hu, K., Zhang, P. and Ma, Z., "A New Simulation Method for 3-D Propellant Grain Burn Analysis of Solid Rocket Motor," 30th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Indianapolis, I.N., AIAA 94-3331, June 1994.