ENH: add structural to total mass ratio for motor and rocket #713
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Lucas-Prates
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Codecov ReportAttention: Patch coverage is
Additional details and impacted files@@ Coverage Diff @@
## develop #713 +/- ##
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+ Coverage 75.88% 75.96% +0.07%
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Files 99 99
Lines 11222 11258 +36
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+ Hits 8516 8552 +36
Misses 2706 2706 ☔ View full report in Codecov by Sentry. |
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Made the suggested changes. The PR is ready for review again! |
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Co-authored-by: Gui-FernandesBR <63590233+Gui-FernandesBR@users.noreply.github.com>
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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).