ENH: add structural to total mass ratio for motor and rocket #713
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Pull request type
Checklist
black rocketpy/ tests/
) has passed locallypytest tests -m slow --runslow
) have passed locallyNew behavior
Solves issue #671 .
Breaking change
Additional information
From what I understood from the issue, the information required to be printed was the the ratio of the dry mass by the total mass. I saw some sources computing the propellant mass ratio, which I believe is the opposite (inverse of the specified ratio).