Work in progress

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    <j.1:description rdf:datatype="http://www.w3.org/1999/02/22-rdf-syntax-ns#HTML">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)</j.1:description>
    <j.0:symbol>R or M_{R}</j.0:symbol>
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    <rdfs:label xml:lang="en">Mass Ratio</rdfs:label>
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    <j.0:iec61360Code>0112/2///62720#UAD109</j.0:iec61360Code>
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<http://qudt.org/vocab/quantitykind/MassRatio>
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  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/FemtoGM-PER-KiloGM> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/GM-PER-GM> ;
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  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/PicoGM-PER-GM> ;
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  <http://qudt.org/schema/qudt/symbol> "R or M_{R}" ;
  rdfs:isDefinedBy <http://qudt.org/2.1/vocab/quantitykind> ;
  rdfs:label "Mass Ratio"@en ;
.

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