@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:FLIGHT-PERFORMANCE-RESERVE-PROPELLANT-MASS
  a qudt:QuantityKind ;
  dcterms:description "A quantity of propellant, at a nominal mixture ratio, along with fuel bias that is set aside from total propellant loaded to cover for statistical variations of flight hardware characteristics and environment conditions on the day of launch. The launch vehicle is designed to accommodate the maximum FPR loading."^^qudt:LatexString ;
  qudt:applicableUnit unit:AMU ;
  qudt:applicableUnit unit:CARAT ;
  qudt:applicableUnit unit:CWT_LONG ;
  qudt:applicableUnit unit:CWT_SHORT ;
  qudt:applicableUnit unit:CentiGM ;
  qudt:applicableUnit unit:DRAM_UK ;
  qudt:applicableUnit unit:DRAM_US ;
  qudt:applicableUnit unit:DWT ;
  qudt:applicableUnit unit:DecaGM ;
  qudt:applicableUnit unit:DeciGM ;
  qudt:applicableUnit unit:DeciTONNE ;
  qudt:applicableUnit unit:DeciTON_Metric ;
  qudt:applicableUnit unit:EarthMass ;
  qudt:applicableUnit unit:FemtoGM ;
  qudt:applicableUnit unit:GM ;
  qudt:applicableUnit unit:GM_Carbon ;
  qudt:applicableUnit unit:GM_DRY ;
  qudt:applicableUnit unit:GM_Nitrogen ;
  qudt:applicableUnit unit:GRAIN ;
  qudt:applicableUnit unit:HectoGM ;
  qudt:applicableUnit unit:Hundredweight_UK ;
  qudt:applicableUnit unit:Hundredweight_US ;
  qudt:applicableUnit unit:KiloGM ;
  qudt:applicableUnit unit:KiloLB ;
  qudt:applicableUnit unit:KiloTONNE ;
  qudt:applicableUnit unit:KiloTON_Metric ;
  qudt:applicableUnit unit:LB ;
  qudt:applicableUnit unit:LB_M ;
  qudt:applicableUnit unit:LB_T ;
  qudt:applicableUnit unit:LunarMass ;
  qudt:applicableUnit unit:MOMME_Pearl ;
  qudt:applicableUnit unit:MOMME_Textile ;
  qudt:applicableUnit unit:MegaGM ;
  qudt:applicableUnit unit:MegaTON ;
  qudt:applicableUnit unit:MegaTONNE ;
  qudt:applicableUnit unit:MicroGM ;
  qudt:applicableUnit unit:MilliGM ;
  qudt:applicableUnit unit:NanoGM ;
  qudt:applicableUnit unit:OZ ;
  qudt:applicableUnit unit:OZ_M ;
  qudt:applicableUnit unit:OZ_TROY ;
  qudt:applicableUnit unit:PENNYWEIGHT ;
  qudt:applicableUnit unit:PFUND ;
  qudt:applicableUnit unit:PicoGM ;
  qudt:applicableUnit unit:PlanckMass ;
  qudt:applicableUnit unit:Quarter_UK ;
  qudt:applicableUnit unit:SLUG ;
  qudt:applicableUnit unit:SolarMass ;
  qudt:applicableUnit unit:Stone_UK ;
  qudt:applicableUnit unit:TON ;
  qudt:applicableUnit unit:TONNE ;
  qudt:applicableUnit unit:TON_Assay ;
  qudt:applicableUnit unit:TON_LONG ;
  qudt:applicableUnit unit:TON_Metric ;
  qudt:applicableUnit unit:TON_SHORT ;
  qudt:applicableUnit unit:TON_UK ;
  qudt:applicableUnit unit:TON_US ;
  qudt:applicableUnit unit:U ;
  qudt:deprecated true ;
  qudt:deprecatedInVersion "3.2.0" ;
  qudt:hasDimensionVector qkdv:A0E0L0I0M1H0T0D0 ;
  qudt:plainTextDescription "A quantity of propellant, at a nominal mixture ratio, along with fuel bias that is set aside from total propellant loaded to cover for statistical variations of flight hardware characteristics and environment conditions on the day of launch. The launch vehicle is designed to accommodate the maximum FPR loading." ;
  rdfs:comment "Applicable units are those of quantitykind:Mass" ;
  rdfs:isDefinedBy <http://qudt.org/3.2.1/vocab/quantitykind> ;
  rdfs:label "Flight Performance Reserve Propellant Mass"@en ;
  skos:altLabel "FPR" ;
  skos:broader quantitykind:Mass .