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A study of the smokeless liner formulation and smoke characteristics  

유지창 (국방과학연구소)
류문삼 (국방과학연구소)
백국현 (국방과학연구소)
류백능 (국방과학연구소)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.6, no.2, 2002 , pp. 19-27 More about this Journal
Abstract
The smokeless liner, was required to propulsion system of gas generator, was developed by appling oxamide as a filler and HTPB system as a binder. Relative quantities of smoke produced during burning of liner by propellant combustion was measured by using smoke chamber. The smoke of the smokeless liner containing 50% of oxamide as filler was reduced to 1/10 as compared with conventional liner containing silica as filler. This result was showed by ground test of gas generator.
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  • Reference
1 A. Davenas, Solid Rocket Propulsion Tecnology, Pergamon Press, Chap. 13, 1993
2 M Pierce et al, U.S. Pat. 4,209,351, Jun. 24, 1980
3 B. Gonthier, Minimum Smoke Rocket Motors with Silicone Inhibitor, AIAA-84-1418, 1984
4 C. I. Evans, 'Minimum Smoke Solid Propellant Motors,' AIAA-72-1192, 1972
5 M. Probster, Propellant, Exprosive, Pyrotechnics, 12, 141, 1987
6 Dale E. Hutchens et al, .U.S. Pat. 6,051,087, Apr. 18, 2000
7 M. Probster, Propellant, Exprosive, pyrotechnics, 13, 157, 1988   DOI   ScienceOn