First, consider a cryogenic chemical propulsion system with . Enter the required propellant fraction as a proportion with at least 2 decimal places (i.e., enter 0.25 to represent 25%):
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I'm atrocious at math, yet this question has come may way nonetheless. Do I just reverse the standard rocket equation one uses to find the Delta Velocity? Propellant/final mass = ΔV x Isp? I need smart folk.
Source https://www.physicsforums.com/threads/need-help-finding-required-propellant-fraction-for-equation.804145/
Explanation:
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