quantitykind:MassRatio

URI: http://qudt.org/vocab/quantitykind/MassRatio

Type
Description

Properties
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)
qudt:symbol
R or M_{R}
Annotations
rdfs:label
Mass Ratio(en)
View as:  CSV

Work in progress

RDF/XML
<rdf:RDF
    xmlns:rdf="http://www.w3.org/1999/02/22-rdf-syntax-ns#"
    xmlns:j.0="http://qudt.org/schema/qudt/"
    xmlns:owl="http://www.w3.org/2002/07/owl#"
    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/PicoGM-PER-GM"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/GM-PER-GM"/>
    <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>
TURTLE
@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://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/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/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:isDefinedBy <http://qudt.org/2.1/vocab/quantitykind> ;
  rdfs:label "Mass Ratio"@en ;
.
JSON
{"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: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" 
    ,"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" 
    ,"isDefinedBy":"&lt;http:\/\/qudt.org\/2.1\/vocab\/quantitykind&gt;" 
    ,"label":"Mass Ratio" 
    ,"symbol":"R or M_{R}" 
    ,"type":"qudt:QuantityKind" 
    ]}
JSON-LD
{
  "@id" : "http://qudt.org/vocab/quantitykind/MassRatio",
  "@type" : "http://qudt.org/schema/qudt/QuantityKind",
  "applicableUnit" : [ "http://qudt.org/vocab/unit/MilliGM-PER-GM", "http://qudt.org/vocab/unit/MilliGM-PER-KiloGM", "http://qudt.org/vocab/unit/FemtoGM-PER-KiloGM", "http://qudt.org/vocab/unit/MicroGM-PER-KiloGM", "http://qudt.org/vocab/unit/PicoGM-PER-GM", "http://qudt.org/vocab/unit/GM-PER-GM", "http://qudt.org/vocab/unit/GM-PER-KiloGM", "http://qudt.org/vocab/unit/MicroGM-PER-GM", "http://qudt.org/vocab/unit/KiloGM-PER-KiloGM", "http://qudt.org/vocab/unit/NanoGM-PER-KiloGM", "http://qudt.org/vocab/unit/PicoGM-PER-KiloGM" ],
  "hasDimensionVector" : "http://qudt.org/vocab/dimensionvector/A0E0L0I0M0H0T0D1",
  "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)",
  "symbol" : "R or M_{R}",
  "isDefinedBy" : "http://qudt.org/2.1/vocab/quantitykind",
  "label" : {
    "@language" : "en",
    "@value" : "Mass Ratio"
  },
  "@context" : {
    "applicableUnit" : {
      "@id" : "http://qudt.org/schema/qudt/applicableUnit",
      "@type" : "@id"
    },
    "symbol" : {
      "@id" : "http://qudt.org/schema/qudt/symbol"
    },
    "plainTextDescription" : {
      "@id" : "http://qudt.org/schema/qudt/plainTextDescription"
    },
    "label" : {
      "@id" : "http://www.w3.org/2000/01/rdf-schema#label"
    },
    "isDefinedBy" : {
      "@id" : "http://www.w3.org/2000/01/rdf-schema#isDefinedBy",
      "@type" : "@id"
    },
    "hasDimensionVector" : {
      "@id" : "http://qudt.org/schema/qudt/hasDimensionVector",
      "@type" : "@id"
    },
    "rdf" : "http://www.w3.org/1999/02/22-rdf-syntax-ns#",
    "owl" : "http://www.w3.org/2002/07/owl#",
    "xsd" : "http://www.w3.org/2001/XMLSchema#",
    "rdfs" : "http://www.w3.org/2000/01/rdf-schema#"
  }
}

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