This HTML5 document contains 17 embedded RDF statements represented using HTML+Microdata notation.

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Namespace Prefixes

Prefix	IRI
n2	http://qudt.org/vocab/quantitykind/
n4	http://qudt.org/vocab/unit/
n3	http://qudt.org/schema/qudt/
n7	http://qudt.org/vocab/dimensionvector/
rdfs	http://www.w3.org/2000/01/rdf-schema#
n6	http://qudt.org/2.1/vocab/
rdf	http://www.w3.org/1999/02/22-rdf-syntax-ns#
xsdh	http://www.w3.org/2001/XMLSchema#

Statements

Subject Item

n2:MassRatio

rdf:type

n3:QuantityKind

rdfs:label

Mass Ratio

rdfs:isDefinedBy

n6:quantitykind

n3:applicableUnit

n4:MicroGM-PER-GM n4:MicroGM-PER-KiloGM n4:GM-PER-GM n4:KiloGM-PER-KiloGM n4:MilliGM-PER-KiloGM n4:GM-PER-KiloGM n4:NanoGM-PER-KiloGM n4:PicoGM-PER-GM n4:PicoGM-PER-KiloGM n4:MilliGM-PER-GM n4:FemtoGM-PER-KiloGM

n3:hasDimensionVector

n7:A0E0L0I0M0H0T0D1

n3:plainTextDescription

In aerospace engineering, mass ratio is a measure of the efficiency of a rocket. It describes how much more massive the vehicle is with propellant than without; that is, it is the ratio of the rocket's wet mass (vehicle plus contents plus propellant) to its dry mass (vehicle plus contents)

n3:symbol

R or M_{R}