I propose the hydrogen cyanide - fluorine rocket.

It has the fabulous potential for a vacuum Isp of up to 380s, with a propellant mix density of 1023 kg/m^3, handily beating methalox mixes. It is non-cryogenic and burns at over 4000K.

Exhaust is 43.3% hydrogen fluoride.

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  • Corkyskog
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    16 hours ago

    How much of a war crime would it be to gift a missile with this as its propulsion system to a foreign nation you don’t like?