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I wanted to know what the most power full solid rocket fuel is. I do not mean theoretical once like metallic hydrogen.

Are solid rocket fuel mixtures prepared in a non-ideal mixture? In other words, do they have to deviate from their stoichiometric ratio in order to have operable temperature and stay under the constraints of the material (or the nozzle is preferably made from an ablative material?)

I want to know the combustion temperatures of solid fuels. Are there any tables or graphs which compare different solid fuels with their respective combustion temperatures?

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    $\begingroup$ Welcome to Space Exploration. Please read our tour and How to Ask pages to understand what we need in a question post, and then edit your post to focus on 1 specific question. As it stands, it is unclear what you are wanting.. $\endgroup$
    – Rory Alsop
    Commented Oct 21, 2022 at 17:57
  • $\begingroup$ ISP 295.2 according to this list. 297 according to this. There could be others. $\endgroup$
    – AJN
    Commented Oct 22, 2022 at 3:59

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