Work in progress

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    xmlns:rdfs="http://www.w3.org/2000/01/rdf-schema#"
    xmlns:xsd="http://www.w3.org/2001/XMLSchema#" > 
  <rdf:Description rdf:about="http://qudt.org/vocab/quantitykind/MassRatio">
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MilliGM-PER-GM"/>
    <j.0:symbol>R or M_{R}</j.0:symbol>
    <j.0:plainTextDescription>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.0:plainTextDescription>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MilliGM-PER-KiloGM"/>
    <rdfs:label xml:lang="en">Mass Ratio</rdfs:label>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/FemtoGM-PER-KiloGM"/>
    <rdf:type rdf:resource="http://qudt.org/schema/qudt/QuantityKind"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MicroGM-PER-KiloGM"/>
    <rdfs:isDefinedBy rdf:resource="http://qudt.org/2.1/vocab/quantitykind"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/LB-PER-LB"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/PicoGM-PER-GM"/>
    <j.0:iec61360Code>0112/2///62720#UAD109</j.0:iec61360Code>
    <rdfs:comment>Applicable units are those of quantitykind:MassRatio</rdfs:comment>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/GM-PER-GM"/>
    <j.1:description rdf:datatype="http://qudt.org/schema/qudt/LatexString">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:applicableUnit rdf:resource="http://qudt.org/vocab/unit/GM-PER-KiloGM"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MicroGM-PER-GM"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/KiloGM-PER-KiloGM"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/NanoGM-PER-KiloGM"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/PicoGM-PER-KiloGM"/>
    <j.0:hasDimensionVector rdf:resource="http://qudt.org/vocab/dimensionvector/A0E0L0I0M0H0T0D1"/>
  </rdf:Description>
</rdf:RDF>

@prefix owl: <http://www.w3.org/2002/07/owl#> .
@prefix rdf: <http://www.w3.org/1999/02/22-rdf-syntax-ns#> .
@prefix rdfs: <http://www.w3.org/2000/01/rdf-schema#> .
@prefix xsd: <http://www.w3.org/2001/XMLSchema#> .

<http://qudt.org/vocab/quantitykind/MassRatio>
  rdf:type <http://qudt.org/schema/qudt/QuantityKind> ;
  <http://purl.org/dc/terms/description> "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)"^^<http://qudt.org/schema/qudt/LatexString> ;
  <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> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/GM-PER-KiloGM> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/KiloGM-PER-KiloGM> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/LB-PER-LB> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MicroGM-PER-GM> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MicroGM-PER-KiloGM> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MilliGM-PER-GM> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MilliGM-PER-KiloGM> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/NanoGM-PER-KiloGM> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/PicoGM-PER-GM> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/PicoGM-PER-KiloGM> ;
  <http://qudt.org/schema/qudt/hasDimensionVector> <http://qudt.org/vocab/dimensionvector/A0E0L0I0M0H0T0D1> ;
  <http://qudt.org/schema/qudt/iec61360Code> "0112/2///62720#UAD109" ;
  <http://qudt.org/schema/qudt/plainTextDescription> "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)" ;
  <http://qudt.org/schema/qudt/symbol> "R or M_{R}" ;
  rdfs:comment "Applicable units are those of quantitykind:MassRatio" ;
  rdfs:isDefinedBy <http://qudt.org/2.1/vocab/quantitykind> ;
  rdfs:label "Mass Ratio"@en ;
.

{"resource":"Mass Ratio" 
 ,"qname":"quantitykind:MassRatio" 
 ,"uri":"http:\/\/qudt.org\/vocab\/quantitykind\/MassRatio" 
 ,"properties":["applicable unit":"unit:FemtoGM-PER-KiloGM" 
    ,"applicable unit":"unit:GM-PER-GM" 
    ,"applicable unit":"unit:GM-PER-KiloGM" 
    ,"applicable unit":"unit:KiloGM-PER-KiloGM" 
    ,"applicable unit":"unit:LB-PER-LB" 
    ,"applicable unit":"unit:MicroGM-PER-GM" 
    ,"applicable unit":"unit:MicroGM-PER-KiloGM" 
    ,"applicable unit":"unit:MilliGM-PER-GM" 
    ,"applicable unit":"unit:MilliGM-PER-KiloGM" 
    ,"applicable unit":"unit:NanoGM-PER-KiloGM" 
    ,"applicable unit":"unit:PicoGM-PER-GM" 
    ,"applicable unit":"unit:PicoGM-PER-KiloGM" 
    ,"comment":"Applicable units are those of quantitykind:MassRatio" 
    ,"description":"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)" 
    ,"description (plain text)":"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)" 
    ,"has dimension vector":"dimension:A0E0L0I0M0H0T0D1" 
    ,"iec-61360 code":"0112\/2\/\/\/62720#UAD109" 
    ,"isDefinedBy":"<http:\/\/qudt.org\/2.1\/vocab\/quantitykind>" 
    ,"label":"Mass Ratio" 
    ,"symbol":"R or M_{R}" 
    ,"type":"qudt:QuantityKind" 
    ]}

{
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  "description" : "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)",
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  "symbol" : "R or M_{R}",
  "comment" : "Applicable units are those of quantitykind:MassRatio",
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  "label" : {
    "@language" : "en",
    "@value" : "Mass Ratio"
  },
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