@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#> .
@prefix owl: <http://www.w3.org/2002/07/owl#> .
@prefix constant: <http://qudt.org/vocab/constant/> .
@prefix dc: <http://purl.org/dc/elements/1.1/> .
@prefix dcterms: <http://purl.org/dc/terms/> .
@prefix prov: <http://www.w3.org/ns/prov#> .
@prefix qkdv: <http://qudt.org/vocab/dimensionvector/> .
@prefix quantitykind: <http://qudt.org/vocab/quantitykind/> .
@prefix qudt: <http://qudt.org/schema/qudt/> .
@prefix si-quantity: <https://si-digital-framework.org/quantities/> .
@prefix skos: <http://www.w3.org/2004/02/skos/core#> .
@prefix unit: <http://qudt.org/vocab/unit/> .
@prefix vaem: <http://www.linkedmodel.org/schema/vaem#> .
@prefix voag: <http://voag.linkedmodel.org/schema/voag#> .

quantitykind:MassRatio
  a qudt:QuantityKind ;
  dcterms: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)"^^qudt:LatexString ;
  qudt:applicableUnit unit:FemtoGM-PER-KiloGM ;
  qudt:applicableUnit unit:GM-PER-GM ;
  qudt:applicableUnit unit:GM-PER-HectoGM ;
  qudt:applicableUnit unit:GM-PER-KiloGM ;
  qudt:applicableUnit unit:KiloGM-PER-KiloGM ;
  qudt:applicableUnit unit:LB-PER-LB ;
  qudt:applicableUnit unit:MicroGM-PER-GM ;
  qudt:applicableUnit unit:MicroGM-PER-KiloGM ;
  qudt:applicableUnit unit:MicroGM-PER-MilliGM ;
  qudt:applicableUnit unit:MilliGM-PER-GM ;
  qudt:applicableUnit unit:MilliGM-PER-KiloGM ;
  qudt:applicableUnit unit:NanoGM-PER-KiloGM ;
  qudt:applicableUnit unit:NanoGM-PER-MilliGM ;
  qudt:applicableUnit unit:PicoGM-PER-GM ;
  qudt:applicableUnit unit:PicoGM-PER-KiloGM ;
  qudt:applicableUnit unit:PicoGM-PER-MilliGM ;
  qudt:hasDimensionVector qkdv:A0E0L0I0M0H0T0D1 ;
  qudt:iec61360Code "0112/2///62720#UAD109" ;
  qudt:informativeReference "https://cdd.iec.ch/cdd/iec61987/iec61987.nsf/ListsOfUnitsAllVersions/0112-2---62720%23UAD109"^^xsd:anyURI ;
  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}" ;
  qudt:wikidataMatch <http://www.wikidata.org/entity/Q1563068> ;
  rdfs:comment "Applicable units are those of quantitykind:MassRatio" ;
  rdfs:isDefinedBy <http://qudt.org/3.1.11/vocab/quantitykind> ;
  rdfs:label "Mass Ratio"@en .