Work in progress

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  <rdf:Description rdf:about="http://qudt.org/vocab/quantitykind/EffectiveExhaustVelocity">
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/CentiM-PER-YR"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/KiloM-PER-DAY"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/KiloM-PER-SEC"/>
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    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/M-PER-HR"/>
    <j.1:description rdf:datatype="http://qudt.org/schema/qudt/LatexString">The velocity of an exhaust stream after reduction by effects such as friction, non-axially directed flow, and pressure differences between the inside of the rocket and its surroundings. The effective exhaust velocity is one of two factors determining the thrust, or accelerating force, that a rocket can develop, the other factor being the quantity of reaction mass expelled from the rocket in unit time. In most cases, the effective exhaust velocity is close to the actual exhaust velocity.</j.1:description>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MI-PER-SEC"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/CentiM-PER-SEC"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/IN-PER-MIN"/>
    <j.0:plainTextDescription>The velocity of an exhaust stream after reduction by effects such as friction, non-axially directed flow, and pressure differences between the inside of the rocket and its surroundings. The effective exhaust velocity is one of two factors determining the thrust, or accelerating force, that a rocket can develop, the other factor being the quantity of reaction mass expelled from the rocket in unit time. In most cases, the effective exhaust velocity is close to the actual exhaust velocity.</j.0:plainTextDescription>
    <rdf:type rdf:resource="http://qudt.org/schema/qudt/QuantityKind"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MI-PER-HR"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/YD-PER-SEC"/>
    <rdfs:label xml:lang="en">Effective Exhaustvelocity</rdfs:label>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/FT-PER-SEC"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MI_N-PER-MIN"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MilliM-PER-DAY"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MilliM-PER-HR"/>
    <j.0:hasDimensionVector rdf:resource="http://qudt.org/vocab/dimensionvector/A0E0L1I0M0H0T-1D0"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/FT-PER-DAY"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/FT-PER-HR"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/CentiM-PER-HR"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/YD-PER-HR"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MI_N-PER-HR"/>
    <rdfs:comment>Applicable units are those of quantitykind:Velocity</rdfs:comment>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/GigaHZ-M"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/YD-PER-MIN"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/CentiM-PER-KiloYR"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/KiloM-PER-HR"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MilliM-PER-MIN"/>
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    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MicroM-PER-SEC"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MI-PER-MIN"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/M-PER-SEC"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/M-PER-MIN"/>
    <j.0:symbol>v_{e}</j.0:symbol>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/IN-PER-YR"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MicroM-PER-MIN"/>
    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/MilliM-PER-YR"/>
    <j.2:broader rdf:resource="http://qudt.org/vocab/quantitykind/Velocity"/>
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    <j.0:applicableUnit rdf:resource="http://qudt.org/vocab/unit/FT-PER-MIN"/>
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@prefix rdf: <http://www.w3.org/1999/02/22-rdf-syntax-ns#> .
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@prefix xsd: <http://www.w3.org/2001/XMLSchema#> .

<http://qudt.org/vocab/quantitykind/EffectiveExhaustVelocity>
  rdf:type <http://qudt.org/schema/qudt/QuantityKind> ;
  <http://purl.org/dc/terms/description> "The velocity of an exhaust stream after reduction by effects such as friction, non-axially directed flow, and pressure differences between the inside of the rocket and its surroundings. The effective exhaust velocity is one of two factors determining the thrust, or accelerating force, that a rocket can develop, the other factor being the quantity of reaction mass expelled from the rocket in unit time. In most cases, the effective exhaust velocity is close to the actual exhaust velocity."^^<http://qudt.org/schema/qudt/LatexString> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/CentiM-PER-HR> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/CentiM-PER-KiloYR> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/CentiM-PER-SEC> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/CentiM-PER-YR> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/FT-PER-DAY> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/FT-PER-HR> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/FT-PER-MIN> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/FT-PER-SEC> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/GigaHZ-M> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/IN-PER-MIN> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/IN-PER-SEC> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/IN-PER-YR> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/KN> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/KiloM-PER-DAY> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/KiloM-PER-HR> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/KiloM-PER-SEC> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/M-PER-HR> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/M-PER-MIN> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/M-PER-SEC> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/M-PER-YR> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MI-PER-HR> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MI-PER-MIN> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MI-PER-SEC> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MI_N-PER-HR> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MI_N-PER-MIN> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MicroM-PER-MIN> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MicroM-PER-SEC> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MilliM-PER-DAY> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MilliM-PER-HR> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MilliM-PER-MIN> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MilliM-PER-SEC> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/MilliM-PER-YR> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/YD-PER-HR> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/YD-PER-MIN> ;
  <http://qudt.org/schema/qudt/applicableUnit> <http://qudt.org/vocab/unit/YD-PER-SEC> ;
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  <http://qudt.org/schema/qudt/plainTextDescription> "The velocity of an exhaust stream after reduction by effects such as friction, non-axially directed flow, and pressure differences between the inside of the rocket and its surroundings. The effective exhaust velocity is one of two factors determining the thrust, or accelerating force, that a rocket can develop, the other factor being the quantity of reaction mass expelled from the rocket in unit time. In most cases, the effective exhaust velocity is close to the actual exhaust velocity." ;
  <http://qudt.org/schema/qudt/symbol> "v_{e}" ;
  rdfs:comment "Applicable units are those of quantitykind:Velocity" ;
  rdfs:isDefinedBy <http://qudt.org/2.1/vocab/quantitykind> ;
  rdfs:label "Effective Exhaustvelocity"@en ;
  <http://www.w3.org/2004/02/skos/core#broader> <http://qudt.org/vocab/quantitykind/Velocity> ;
.

{"resource":"Effective Exhaustvelocity" 
 ,"qname":"quantitykind:EffectiveExhaustVelocity" 
 ,"uri":"http:\/\/qudt.org\/vocab\/quantitykind\/EffectiveExhaustVelocity" 
 ,"properties":["applicable unit":"unit:CentiM-PER-HR" 
    ,"applicable unit":"unit:CentiM-PER-KiloYR" 
    ,"applicable unit":"unit:CentiM-PER-SEC" 
    ,"applicable unit":"unit:CentiM-PER-YR" 
    ,"applicable unit":"unit:FT-PER-DAY" 
    ,"applicable unit":"unit:FT-PER-HR" 
    ,"applicable unit":"unit:FT-PER-MIN" 
    ,"applicable unit":"unit:FT-PER-SEC" 
    ,"applicable unit":"unit:GigaHZ-M" 
    ,"applicable unit":"unit:IN-PER-MIN" 
    ,"applicable unit":"unit:IN-PER-SEC" 
    ,"applicable unit":"unit:IN-PER-YR" 
    ,"applicable unit":"unit:KN" 
    ,"applicable unit":"unit:KiloM-PER-DAY" 
    ,"applicable unit":"unit:KiloM-PER-HR" 
    ,"applicable unit":"unit:KiloM-PER-SEC" 
    ,"applicable unit":"unit:M-PER-HR" 
    ,"applicable unit":"unit:M-PER-MIN" 
    ,"applicable unit":"unit:M-PER-SEC" 
    ,"applicable unit":"unit:M-PER-YR" 
    ,"applicable unit":"unit:MI-PER-HR" 
    ,"applicable unit":"unit:MI-PER-MIN" 
    ,"applicable unit":"unit:MI-PER-SEC" 
    ,"applicable unit":"unit:MI_N-PER-HR" 
    ,"applicable unit":"unit:MI_N-PER-MIN" 
    ,"applicable unit":"unit:MicroM-PER-MIN" 
    ,"applicable unit":"unit:MicroM-PER-SEC" 
    ,"applicable unit":"unit:MilliM-PER-DAY" 
    ,"applicable unit":"unit:MilliM-PER-HR" 
    ,"applicable unit":"unit:MilliM-PER-MIN" 
    ,"applicable unit":"unit:MilliM-PER-SEC" 
    ,"applicable unit":"unit:MilliM-PER-YR" 
    ,"applicable unit":"unit:YD-PER-HR" 
    ,"applicable unit":"unit:YD-PER-MIN" 
    ,"applicable unit":"unit:YD-PER-SEC" 
    ,"comment":"Applicable units are those of quantitykind:Velocity" 
    ,"description":"The velocity of an exhaust stream after reduction by effects such as friction, non-axially directed flow, and pressure differences between the inside of the rocket and its surroundings. The effective exhaust velocity is one of two factors determining the thrust, or accelerating force, that a rocket can develop, the other factor being the quantity of reaction mass expelled from the rocket in unit time. In most cases, the effective exhaust velocity is close to the actual exhaust velocity." 
    ,"description (plain text)":"The velocity of an exhaust stream after reduction by effects such as friction, non-axially directed flow, and pressure differences between the inside of the rocket and its surroundings. The effective exhaust velocity is one of two factors determining the thrust, or accelerating force, that a rocket can develop, the other factor being the quantity of reaction mass expelled from the rocket in unit time. In most cases, the effective exhaust velocity is close to the actual exhaust velocity." 
    ,"has broader":"quantitykind:Velocity" 
    ,"has dimension vector":"dimension:A0E0L1I0M0H0T-1D0" 
    ,"isDefinedBy":"<http:\/\/qudt.org\/2.1\/vocab\/quantitykind>" 
    ,"label":"Effective Exhaustvelocity" 
    ,"symbol":"v_{e}" 
    ,"type":"qudt:QuantityKind" 
    ]}

{
  "@id" : "http://qudt.org/vocab/quantitykind/EffectiveExhaustVelocity",
  "@type" : "http://qudt.org/schema/qudt/QuantityKind",
  "description" : "The velocity of an exhaust stream after reduction by effects such as friction, non-axially directed flow, and pressure differences between the inside of the rocket and its surroundings. The effective exhaust velocity is one of two factors determining the thrust, or accelerating force, that a rocket can develop, the other factor being the quantity of reaction mass expelled from the rocket in unit time. In most cases, the effective exhaust velocity is close to the actual exhaust velocity.",
  "applicableUnit" : [ "http://qudt.org/vocab/unit/CentiM-PER-YR", "http://qudt.org/vocab/unit/KiloM-PER-DAY", "http://qudt.org/vocab/unit/KiloM-PER-SEC", "http://qudt.org/vocab/unit/KN", "http://qudt.org/vocab/unit/IN-PER-SEC", "http://qudt.org/vocab/unit/M-PER-HR", "http://qudt.org/vocab/unit/MI-PER-SEC", "http://qudt.org/vocab/unit/CentiM-PER-SEC", "http://qudt.org/vocab/unit/IN-PER-MIN", "http://qudt.org/vocab/unit/MI-PER-HR", "http://qudt.org/vocab/unit/YD-PER-SEC", "http://qudt.org/vocab/unit/FT-PER-SEC", "http://qudt.org/vocab/unit/MI_N-PER-MIN", "http://qudt.org/vocab/unit/MilliM-PER-DAY", "http://qudt.org/vocab/unit/MilliM-PER-HR", "http://qudt.org/vocab/unit/FT-PER-DAY", "http://qudt.org/vocab/unit/FT-PER-HR", "http://qudt.org/vocab/unit/CentiM-PER-HR", "http://qudt.org/vocab/unit/YD-PER-HR", "http://qudt.org/vocab/unit/MI_N-PER-HR", "http://qudt.org/vocab/unit/GigaHZ-M", "http://qudt.org/vocab/unit/YD-PER-MIN", "http://qudt.org/vocab/unit/CentiM-PER-KiloYR", "http://qudt.org/vocab/unit/KiloM-PER-HR", "http://qudt.org/vocab/unit/MilliM-PER-MIN", "http://qudt.org/vocab/unit/MicroM-PER-SEC", "http://qudt.org/vocab/unit/MI-PER-MIN", "http://qudt.org/vocab/unit/M-PER-SEC", "http://qudt.org/vocab/unit/M-PER-MIN", "http://qudt.org/vocab/unit/IN-PER-YR", "http://qudt.org/vocab/unit/MicroM-PER-MIN", "http://qudt.org/vocab/unit/MilliM-PER-YR", "http://qudt.org/vocab/unit/MilliM-PER-SEC", "http://qudt.org/vocab/unit/M-PER-YR", "http://qudt.org/vocab/unit/FT-PER-MIN" ],
  "hasDimensionVector" : "http://qudt.org/vocab/dimensionvector/A0E0L1I0M0H0T-1D0",
  "plainTextDescription" : "The velocity of an exhaust stream after reduction by effects such as friction, non-axially directed flow, and pressure differences between the inside of the rocket and its surroundings. The effective exhaust velocity is one of two factors determining the thrust, or accelerating force, that a rocket can develop, the other factor being the quantity of reaction mass expelled from the rocket in unit time. In most cases, the effective exhaust velocity is close to the actual exhaust velocity.",
  "symbol" : "v_{e}",
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  "isDefinedBy" : "http://qudt.org/2.1/vocab/quantitykind",
  "label" : {
    "@language" : "en",
    "@value" : "Effective Exhaustvelocity"
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