Definition

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)

Concept Hierarchy

Current Concept

Concept Information

IRI

https://vocab.sentie...ntity-kind/MassRatio

Notation

0112/2///62720#UAD109

Status

Accepted