quantitykind:SpecificImpulse

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

Type
Description

The impulse produced by a rocket divided by the mass \(mp\) of propellant consumed. Specific impulse \({I_{sp}}\) is a widely used measure of performance for chemical, nuclear, and electric rockets. It is usually given in seconds for both U.S. Customary and International System (SI) units. The impulse produced by a rocket is the thrust force \(F\) times its duration \(t\) in seconds. \(I_{sp}\) is the thrust per unit mass flowrate, but with \(g_o\), is the thrust per weight flowrate. The specific impulse is given by the equation: \(I_{sp} = \frac{F}{\dot{m}g_o}\).

Properties
Annotations
dcterms:description
The impulse produced by a rocket divided by the mass \(mp\) of propellant consumed. Specific impulse \({I_{sp}}\) is a widely used measure of performance for chemical, nuclear, and electric rockets. It is usually given in seconds for both U.S. Customary and International System (SI) units. The impulse produced by a rocket is the thrust force \(F\) times its duration \(t\) in seconds. \(I_{sp}\) is the thrust per unit mass flowrate, but with \(g_o\), is the thrust per weight flowrate. The specific impulse is given by the equation: \(I_{sp} = \frac{F}{\dot{m}g_o}\).
rdfs:label
Specific Impulse(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:j.1="http://purl.org/dc/terms/"
    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/SpecificImpulse">
    <rdf:type rdf:resource="http://qudt.org/schema/qudt/QuantityKind"/>
    <j.1:description rdf:datatype="http://qudt.org/schema/qudt/LatexString">The impulse produced by a rocket divided by the mass \(mp\) of propellant consumed. Specific impulse \({I_{sp}}\) is a widely used measure of performance for chemical, nuclear, and electric rockets. It is usually given in seconds for both U.S. Customary and International System (SI) units.  The impulse produced by a rocket is the thrust force \(F\) times its duration \(t\) in seconds. \(I_{sp}\) is the thrust per unit mass flowrate, but with \(g_o\), is the thrust per weight flowrate. The specific impulse is given by the equation: \(I_{sp} = \frac{F}{\dot{m}g_o}\).</j.1:description>
    <j.0:hasDimensionVector rdf:resource="http://qudt.org/vocab/dimensionvector/A0E0L0I0M0H0T1D0"/>
    <j.0:informativeReference rdf:datatype="http://www.w3.org/2001/XMLSchema#anyURI">http://www.grc.nasa.gov/WWW/K-12/airplane/specimp.html</j.0:informativeReference>
    <rdfs:isDefinedBy rdf:resource="http://qudt.org/2.1/vocab/quantitykind"/>
    <rdfs:label xml:lang="en">Specific Impulse</rdfs:label>
    <rdfs:seeAlso rdf:resource="http://qudt.org/vocab/quantitykind/MassFlowRate"/>
  </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/SpecificImpulse>
  rdf:type <http://qudt.org/schema/qudt/QuantityKind> ;
  <http://purl.org/dc/terms/description> "The impulse produced by a rocket divided by the mass \\(mp\\) of propellant consumed. Specific impulse \\({I_{sp}}\\) is a widely used measure of performance for chemical, nuclear, and electric rockets. It is usually given in seconds for both U.S. Customary and International System (SI) units.  The impulse produced by a rocket is the thrust force \\(F\\) times its duration \\(t\\) in seconds. \\(I_{sp}\\) is the thrust per unit mass flowrate, but with \\(g_o\\), is the thrust per weight flowrate. The specific impulse is given by the equation: \\(I_{sp} = \\frac{F}{\\dot{m}g_o}\\)."^^<http://qudt.org/schema/qudt/LatexString> ;
  <http://qudt.org/schema/qudt/hasDimensionVector> <http://qudt.org/vocab/dimensionvector/A0E0L0I0M0H0T1D0> ;
  <http://qudt.org/schema/qudt/informativeReference> "http://www.grc.nasa.gov/WWW/K-12/airplane/specimp.html"^^xsd:anyURI ;
  rdfs:isDefinedBy <http://qudt.org/2.1/vocab/quantitykind> ;
  rdfs:label "Specific Impulse"@en ;
  rdfs:seeAlso <http://qudt.org/vocab/quantitykind/MassFlowRate> ;
.
JSON
{"resource":"Specific Impulse" 
 ,"qname":"quantitykind:SpecificImpulse" 
 ,"uri":"http:\/\/qudt.org\/vocab\/quantitykind\/SpecificImpulse" 
 ,"properties":["description":"The impulse produced by a rocket divided by the mass \\(mp\\) of propellant consumed. Specific impulse \\({I_{sp}}\\) is a widely used measure of performance for chemical, nuclear, and electric rockets. It is usually given in seconds for both U.S. Customary and International System (SI) units.  The impulse produced by a rocket is the thrust force \\(F\\) times its duration \\(t\\) in seconds. \\(I_{sp}\\) is the thrust per unit mass flowrate, but with \\(g_o\\), is the thrust per weight flowrate. The specific impulse is given by the equation: \\(I_{sp} = \\frac{F}{\\dot{m}g_o}\\)." 
    ,"has dimension vector":"dimension:A0E0L0I0M0H0T1D0" 
    ,"informative reference":"http:\/\/www.grc.nasa.gov\/WWW\/K-12\/airplane\/specimp.html" 
    ,"isDefinedBy":"&lt;http:\/\/qudt.org\/2.1\/vocab\/quantitykind&gt;" 
    ,"label":"Specific Impulse" 
    ,"seeAlso":"quantitykind:MassFlowRate" 
    ,"type":"qudt:QuantityKind" 
    ]}
JSON-LD
{
  "@id" : "http://qudt.org/vocab/quantitykind/SpecificImpulse",
  "@type" : "http://qudt.org/schema/qudt/QuantityKind",
  "description" : "The impulse produced by a rocket divided by the mass \\(mp\\) of propellant consumed. Specific impulse \\({I_{sp}}\\) is a widely used measure of performance for chemical, nuclear, and electric rockets. It is usually given in seconds for both U.S. Customary and International System (SI) units.  The impulse produced by a rocket is the thrust force \\(F\\) times its duration \\(t\\) in seconds. \\(I_{sp}\\) is the thrust per unit mass flowrate, but with \\(g_o\\), is the thrust per weight flowrate. The specific impulse is given by the equation: \\(I_{sp} = \\frac{F}{\\dot{m}g_o}\\).",
  "hasDimensionVector" : "http://qudt.org/vocab/dimensionvector/A0E0L0I0M0H0T1D0",
  "informativeReference" : "http://www.grc.nasa.gov/WWW/K-12/airplane/specimp.html",
  "isDefinedBy" : "http://qudt.org/2.1/vocab/quantitykind",
  "label" : {
    "@language" : "en",
    "@value" : "Specific Impulse"
  },
  "seeAlso" : "http://qudt.org/vocab/quantitykind/MassFlowRate",
  "@context" : {
    "description" : {
      "@id" : "http://purl.org/dc/terms/description",
      "@type" : "http://qudt.org/schema/qudt/LatexString"
    },
    "hasDimensionVector" : {
      "@id" : "http://qudt.org/schema/qudt/hasDimensionVector",
      "@type" : "@id"
    },
    "informativeReference" : {
      "@id" : "http://qudt.org/schema/qudt/informativeReference",
      "@type" : "http://www.w3.org/2001/XMLSchema#anyURI"
    },
    "isDefinedBy" : {
      "@id" : "http://www.w3.org/2000/01/rdf-schema#isDefinedBy",
      "@type" : "@id"
    },
    "label" : {
      "@id" : "http://www.w3.org/2000/01/rdf-schema#label"
    },
    "seeAlso" : {
      "@id" : "http://www.w3.org/2000/01/rdf-schema#seeAlso",
      "@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#"
  }
}

Generated 2023-01-13T16:31:48.731-05:00 by lmdoc version 1.1 with  TopBraid SPARQL Web Pages (SWP)