quantitykind:FLIGHT-PERFORMANCE-RESERVE-PROPELLANT-MASS

URI: http://qudt.org/vocab/quantitykind/FLIGHT-PERFORMANCE-RESERVE-PROPELLANT-MASS

Type
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.

Properties
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.
Annotations
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.
rdfs:label
Flight Performance Reserve Propellant Mass(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/"
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    xmlns:xsd="http://www.w3.org/2001/XMLSchema#" > 
  <rdf:Description rdf:about="http://qudt.org/vocab/quantitykind/FLIGHT-PERFORMANCE-RESERVE-PROPELLANT-MASS">
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MilliGM"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/TON_US"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/DeciGM"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/TON_Assay"/>
    <j.1:description rdf:datatype="http://www.w3.org/1999/02/22-rdf-syntax-ns#HTML">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.</j.1:description>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/KiloGM"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/NanoGM"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/LunarMass"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/AMU"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/CentiGM"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/Hundredweight_UK"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MegaGM"/>
    <rdf:type rdf:resource="http://qudt.org/schema/qudt/QuantityKind"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MegaTONNE"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MOMME_Textile"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/OZ_TROY"/>
    <j.0: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.</j.0:plainTextDescription>
    <rdfs:isDefinedBy rdf:resource="http://qudt.org/2.1/vocab/quantitykind"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/GM"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/EarthMass"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/TON_LONG"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/Stone_UK"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/TONNE"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/DRAM_UK"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/OZ_M"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/PlanckMass"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/OZ"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/KiloTONNE"/>
    <j.2:altLabel>FPR</j.2:altLabel>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/CWT_LONG"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/Hundredweight_US"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/PicoGM"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/Pennyweight"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/TON_Metric"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/LB_M"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/PFUND"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MOMME_Pearl"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/CARAT"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/TON"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/DecaGM"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/LB_T"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/LB"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/HectoGM"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/U"/>
    <rdfs:label xml:lang="en">Flight Performance Reserve Propellant Mass</rdfs:label>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/SLUG"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MicroGM"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/Quarter_UK"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/KiloTON_Metric"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/SolarMass"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/GRAIN"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/TON_UK"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/DeciTONNE"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/CWT_SHORT"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/FemtoGM"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MegaTON"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/DWT"/>
    <j.0:hasDimensionVector rdf:resource="http://qudt.org/vocab/dimensionvector/A0E0L0I0M1H0T0D0"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/DRAM_US"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/DeciTON_Metric"/>
    <j.2:broader rdf:resource="http://qudt.org/vocab/quantitykind/Mass"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/TON_SHORT"/>
  </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/FLIGHT-PERFORMANCE-RESERVE-PROPELLANT-MASS>
  rdf:type <http://qudt.org/schema/qudt/QuantityKind> ;
  <http://purl.org/dc/terms/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."^^rdf:HTML ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/AMU> ;
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  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/CentiGM> ;
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  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/EarthMass> ;
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  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/Hundredweight_US> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/KiloGM> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/KiloTONNE> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/KiloTON_Metric> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/LB> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/LB_M> ;
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  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/LunarMass> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MOMME_Pearl> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MOMME_Textile> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MegaGM> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MegaTON> ;
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  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MicroGM> ;
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  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/NanoGM> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/OZ> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/OZ_M> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/OZ_TROY> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/PFUND> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/Pennyweight> ;
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  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/TONNE> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/TON_Assay> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/TON_LONG> ;
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  rdfs:isDefinedBy <http://qudt.org/2.1/vocab/quantitykind> ;
  rdfs:label "Flight Performance Reserve Propellant Mass"@en ;
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.
JSON
{"resource":"Flight Performance Reserve Propellant Mass" 
 ,"qname":"quantitykind:FLIGHT-PERFORMANCE-RESERVE-PROPELLANT-MASS" 
 ,"uri":"http:\/\/qudt.org\/vocab\/quantitykind\/FLIGHT-PERFORMANCE-RESERVE-PROPELLANT-MASS" 
 ,"properties":["alternative label":"FPR" 
    ,"applicable unit":"unit:AMU" 
    ,"applicable unit":"unit:CARAT" 
    ,"applicable unit":"unit:CWT_LONG" 
    ,"applicable unit":"unit:CWT_SHORT" 
    ,"applicable unit":"unit:CentiGM" 
    ,"applicable unit":"unit:DRAM_UK" 
    ,"applicable unit":"unit:DRAM_US" 
    ,"applicable unit":"unit:DWT" 
    ,"applicable unit":"unit:DecaGM" 
    ,"applicable unit":"unit:DeciGM" 
    ,"applicable unit":"unit:DeciTONNE" 
    ,"applicable unit":"unit:DeciTON_Metric" 
    ,"applicable unit":"unit:EarthMass" 
    ,"applicable unit":"unit:FemtoGM" 
    ,"applicable unit":"unit:GM" 
    ,"applicable unit":"unit:GRAIN" 
    ,"applicable unit":"unit:HectoGM" 
    ,"applicable unit":"unit:Hundredweight_UK" 
    ,"applicable unit":"unit:Hundredweight_US" 
    ,"applicable unit":"unit:KiloGM" 
    ,"applicable unit":"unit:KiloTONNE" 
    ,"applicable unit":"unit:KiloTON_Metric" 
    ,"applicable unit":"unit:LB" 
    ,"applicable unit":"unit:LB_M" 
    ,"applicable unit":"unit:LB_T" 
    ,"applicable unit":"unit:LunarMass" 
    ,"applicable unit":"unit:MOMME_Pearl" 
    ,"applicable unit":"unit:MOMME_Textile" 
    ,"applicable unit":"unit:MegaGM" 
    ,"applicable unit":"unit:MegaTON" 
    ,"applicable unit":"unit:MegaTONNE" 
    ,"applicable unit":"unit:MicroGM" 
    ,"applicable unit":"unit:MilliGM" 
    ,"applicable unit":"unit:NanoGM" 
    ,"applicable unit":"unit:OZ" 
    ,"applicable unit":"unit:OZ_M" 
    ,"applicable unit":"unit:OZ_TROY" 
    ,"applicable unit":"unit:PFUND" 
    ,"applicable unit":"unit:Pennyweight" 
    ,"applicable unit":"unit:PicoGM" 
    ,"applicable unit":"unit:PlanckMass" 
    ,"applicable unit":"unit:Quarter_UK" 
    ,"applicable unit":"unit:SLUG" 
    ,"applicable unit":"unit:SolarMass" 
    ,"applicable unit":"unit:Stone_UK" 
    ,"applicable unit":"unit:TON" 
    ,"applicable unit":"unit:TONNE" 
    ,"applicable unit":"unit:TON_Assay" 
    ,"applicable unit":"unit:TON_LONG" 
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    ,"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." 
    ,"description (plain text)":"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." 
    ,"has broader":"quantitykind:Mass" 
    ,"has dimension vector":"dimension:A0E0L0I0M1H0T0D0" 
    ,"isDefinedBy":"&lt;http:\/\/qudt.org\/2.1\/vocab\/quantitykind&gt;" 
    ,"label":"Flight Performance Reserve Propellant Mass" 
    ,"type":"qudt:QuantityKind" 
    ]}
JSON-LD
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  "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.",
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  }
}

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