| Predicate | Object |
|---|---|
rdf:type |
qudt:QuantityKind |
dcterms:description |
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) |
qudt:applicableUnit |
Show 16 values
|
qudt:hasDimensionVector |
qkdv:A0E0L0I0M0H0T0D1 |
qudt:iec61360Code |
“0112/2///62720#UAD109” |
qudt:informativeReference |
https://cdd.iec.ch/cdd/iec61987/iec61987.nsf/ListsOfUnitsAllVersions/0112-2---62720%23UAD109 |
qudt: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)” |
qudt:symbol |
“R or M_{R}” |
qudt:wikidataMatch |
http://www.wikidata.org/entity/Q1563068 |
rdfs:comment |
“Applicable units are those of quantitykind:MassRatio” |
rdfs:isDefinedBy |
http://qudt.org/3.1.10/vocab/quantitykind |
rdfs:label |
“Mass Ratio”@en |