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Sentier.dev Common Units Taxonomy adapted from QUDT 2.1

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Mass Ratio (en)

In aerospace engineering, mass ratio is a measure of the efficiency of a rocket. It describes how much more massive the vehicle is with propellant than without; that is, it is the ratio of the rocket's wet mass (vehicle plus contents plus propellant) to its dry mass (vehicle plus contents)

3H Kilogram per Kilogram (en)

0112/2///62720#UAD109
R or M_{R}

In aerospace engineering, mass ratio is a measure of the efficiency of a rocket. It describes how much more massive the vehicle is with propellant than without; that is, it is the ratio of the rocket's wet mass (vehicle plus contents plus propellant) to its dry mass (vehicle plus contents)

0112/2///62720#UAD109
R or M_{R}
Mass Ratio

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https://vocab.sentier.dev/units/quantity-kind/MassRatio

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