1 |
Merkle, C.L., Turk, S.L., and Summerfield, M., "Extinguishment of Solid Propellants by Rapid Depressurization," PRINCETON UNIV NJ DEPT OF AEROSPACE AND MECHANICAL SCIENCES, 1969.
|
2 |
Clepluch, C.C., “Effect of Rapid Pressure Decay on Solid Propellant Combustion,” ARS Journal, Vol. 31, No. 11, pp. 1584-1586, 1961.
|
3 |
Donde, R. Riva, G. and De Luca, L., “Experimental and theoretical extinction of solid rocket propellants by fast depressurization,” Acta Astrinautica, Vol. 11, No. 9, pp. 569-576, 1984.
DOI
|
4 |
Kim, D.Y., Ko, S.W., Jeong, H.H., and Yoon, W.S., "Depressurization Characteristics Analysis of Combustor for Aluminum Agglomeration Modeling of Solid Propellant," 2017 KSPE Fall Conference, Busan, Korea, pp. 346-347, November 2017.
|
5 |
Choi, J.S., Lee, C.H., Lim, J.I., and Lee, H.J., “A Study on Characteristic of Extinguishment for Solid Propellants Composition by Rapid Depressurization,” Journal of the Korean Society of Propulsion Engineers, Vol. 21, No. 5, pp. 37-45, 2017.
DOI
|
6 |
Boggs, T.L., Derr, R.L., and Beckstead, M.W., “Surface Structure of Ammonium Perchlorate Composite Propellants,” AIAA Journal, Vol. 8, No. 2, pp. 370-372, 1970.
DOI
|
7 |
Hwang, Y.S., “Experimental Study on the Extinction Characteristics of the Solid Propellant,” Journal of the Korean Society of Propulsion Engineers, Vol. 8, No. 3, pp. 61-67, 2004.
|