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Do solid propellants have an optimum temperature to burn effectively?

If so, what is the range of temperature needed?

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closed as too broad by called2voyage, user29 Sep 9 '13 at 16:57

Please edit the question to limit it to a specific problem with enough detail to identify an adequate answer. Avoid asking multiple distinct questions at once. See the How to Ask page for help clarifying this question. If this question can be reworded to fit the rules in the help center, please edit the question.

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    $\begingroup$ 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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    $\begingroup$ @Everyone its about optimum temperature and IMO both questions are not linked $\endgroup$ – Hash Sep 7 '13 at 14:05
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    $\begingroup$ 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

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