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Burning Properties of Uncured HTPB Propellant
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 Title & Authors
Burning Properties of Uncured HTPB Propellant
Kim, Nakhyun; Kim, Jungeun; Hong, Myungpyo;
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 Abstract
In this study, we examined the burning rate of the uncured propellant (with and without a curing agent application) in order to inspect the process of the HTPB solid propellant. The burning rate of the uncured propellant, that did not contain the curing agent, was approximately 9.7 mm/s at 1000 psi. In relation to the curing time, the burning rate was constant. The propellant, with the curing agent application, was approximately 8.1 mm/s showed a tendency of slowing as it burned. When the cure reaction rate was low, in accordance to the time, there were small changes in burn rate. However, when the cure reaction rate was high, the difference in burning rate was increased. The burning rate of a fully-cured propellant was approximately 6.8 mm/s, which appeared to be the lowest in order.
 Keywords
Uncured Propellant;Strand Burner;Burning Rate;
 Language
Korean
 Cited by
 References
1.
Oberth, A.E., Principle of Solid Propellant Development, Chemical Propulsion Information Agency, Baltimore, MD, USA, 1987.

2.
Thakre, P. and Yang, V., Solid Propellants, Encyclopedia of Aerospace Engineering, John Wiley & Sons, Ltd., Chicester, UK, pp. 1-10, 2010.