@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:EffectiveExhaustVelocity
  a qudt:QuantityKind ;
  dcterms: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."^^qudt:LatexString ;
  qudt:applicableUnit unit:CentiM-PER-HR ;
  qudt:applicableUnit unit:CentiM-PER-KiloYR ;
  qudt:applicableUnit unit:CentiM-PER-SEC ;
  qudt:applicableUnit unit:CentiM-PER-YR ;
  qudt:applicableUnit unit:FT-PER-DAY ;
  qudt:applicableUnit unit:FT-PER-HR ;
  qudt:applicableUnit unit:FT-PER-MIN ;
  qudt:applicableUnit unit:FT-PER-SEC ;
  qudt:applicableUnit unit:GigaHZ-M ;
  qudt:applicableUnit unit:IN-PER-MIN ;
  qudt:applicableUnit unit:IN-PER-SEC ;
  qudt:applicableUnit unit:IN-PER-YR ;
  qudt:applicableUnit unit:KN ;
  qudt:applicableUnit unit:KiloM-PER-DAY ;
  qudt:applicableUnit unit:KiloM-PER-HR ;
  qudt:applicableUnit unit:KiloM-PER-SEC ;
  qudt:applicableUnit unit:M-PER-DAY ;
  qudt:applicableUnit unit:M-PER-HR ;
  qudt:applicableUnit unit:M-PER-MIN ;
  qudt:applicableUnit unit:M-PER-SEC ;
  qudt:applicableUnit unit:M-PER-YR ;
  qudt:applicableUnit unit:MI-PER-HR ;
  qudt:applicableUnit unit:MI-PER-MIN ;
  qudt:applicableUnit unit:MI-PER-SEC ;
  qudt:applicableUnit unit:MI_N-PER-HR ;
  qudt:applicableUnit unit:MI_N-PER-MIN ;
  qudt:applicableUnit unit:MicroM-PER-MIN ;
  qudt:applicableUnit unit:MicroM-PER-SEC ;
  qudt:applicableUnit unit:MilliM-PER-DAY ;
  qudt:applicableUnit unit:MilliM-PER-HR ;
  qudt:applicableUnit unit:MilliM-PER-MIN ;
  qudt:applicableUnit unit:MilliM-PER-SEC ;
  qudt:applicableUnit unit:MilliM-PER-YR ;
  qudt:applicableUnit unit:YD-PER-HR ;
  qudt:applicableUnit unit:YD-PER-MIN ;
  qudt:applicableUnit unit:YD-PER-SEC ;
  qudt:hasDimensionVector qkdv:A0E0L1I0M0H0T-1D0 ;
  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." ;
  qudt:symbol "v_{e}" ;
  rdfs:comment "Applicable units are those of quantitykind:Velocity" ;
  rdfs:isDefinedBy <http://qudt.org/3.2.1/vocab/quantitykind> ;
  rdfs:label "Effective Exhaustvelocity"@en ;
  skos:broader quantitykind:Velocity .