Do solid propellants have an optimum temperature to burn effectively?
If so, what is the range of temperature needed?
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1$\begingroup$ Pressure is closely related to temperature. Perhaps this question should be linked space.stackexchange.com/questions/439/… $\endgroup$ – Everyone Sep 7 '13 at 13:30
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2$\begingroup$ @Everyone its about optimum temperature and IMO both questions are not linked $\endgroup$ – Hash Sep 7 '13 at 14:05
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1$\begingroup$ Varies greatly based on propellant and engine types, a range is effectively meaningless in this broad context. "Optimum temperature" is unclear too, how broad of a range can still be an "optimum temperature"? $\endgroup$ – called2voyage♦ Sep 9 '13 at 15:55
