@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:SpecificThrust
  a qudt:QuantityKind ;
  dcterms:description """Specific impulse (usually abbreviated Isp) is a way to describe the efficiency of rocket and jet engines.
    It represents the force with respect to the amount of propellant used per unit time.[1] If the "amount" of propellant is given
    in terms of mass (such as kilograms), then specific impulse has units of velocity. If it is given in terms of Earth-weight
    (such as kiloponds), then specific impulse has units of time. The conversion constant between the two versions of specific
    impulse is g. The higher the specific impulse, the lower the propellant flow rate required for a given thrust, and in the case
    of a rocket the less propellant is needed for a given delta-v per the Tsiolkovsky rocket equation.
  """^^qudt:LatexString ;
  qudt:dbpediaMatch "http://dbpedia.org/resource/Specific_thrust"^^xsd:anyURI ;
  qudt:hasDimensionVector qkdv:A0E0L1I0M0H0T-1D0 ;
  qudt:id "Q-160-100" ;
  qudt:informativeReference "https://en.wikipedia.org/wiki/Specific_thrust"^^xsd:anyURI ;
  qudt:plainTextDescription """Specific impulse (usually abbreviated Isp) is a way to describe the efficiency of rocket and jet
    engines. It represents the force with respect to the amount of propellant used per unit time.[1] If the "amount" of propellant
    is given in terms of mass (such as kilograms), then specific impulse has units of velocity. If it is given in terms of
    Earth-weight (such as kiloponds), then specific impulse has units of time. The conversion constant between the two versions of
    specific impulse is g. The higher the specific impulse, the lower the propellant flow rate required for a given thrust, and in
    the case of a rocket the less propellant is needed for a given delta-v per the Tsiolkovsky rocket equation.
  """ ;
  rdfs:isDefinedBy <http://qudt.org/3.4.0/vocab/quantitykind> ;
  rdfs:label "Specific Thrust"@en ;
  rdfs:seeAlso quantitykind:SpecificImpulse .