1 |
Hodge, K., Crofoot, T. and Nelson, S., "Gelled propellants for tactical missile applications," 35th Joint Propulsion Conference and Exhibit, Los Angeles, C.A., U.S.A., AIAA 1999-2976, Jun. 1990.
|
2 |
Stadler, L., Hoffmann, S., Huber, J., Naumann, K. and Stingl, R., "The flight demonstration of the double pulse motor demonstrator MSA," 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Nashvile, T.N., U.S.A., AIAA 2010-6756, Jul. 2010.
|
3 |
Mongia, H.C. and Ambs, L.L., "A Model for the combustion and extinction of composite solid propellants during depressurization," Combustion and Flame, Vol. 22, No. 1, pp. 59-69, 1974.
DOI
|
4 |
T'ien, J.S., "Theoretical criterion for dynamic extinction of solid propellants by fast depressurization," Combustion science and technology, Vol. 9, Issue 1-2, pp. 37-39, 1974.
DOI
|
5 |
Donde, R., Riva, G. and Luca, L.D., "Experimental and theoretical extinction of solid rocket propellants by fast depressurization," Acta Astronautica, Vol. 11, No. 9, pp. 569-576, 1984.
DOI
|
6 |
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.
|
7 |
Jeong, H.G. and Lee, C.J., "Dynamic Extinction of Solid Propellants by Depressurization of Combustion Chamber," Journal of the Korean Society for Aeronautical & Space Sciences, Vol. 30, No. 2, pp. 91-97, 2002.
DOI
|
8 |
Carl, C.C., "Effect of Composition on Combustion of Solid Propellants during a Rapid Pressure Decrease," NASA TM-D1559, 1962.
|