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Namespace Prefixes

PrefixIRI
n2http://qudt.org/vocab/quantitykind/
n4http://qudt.org/vocab/unit/
n3http://qudt.org/schema/qudt/
n6http://qudt.org/vocab/dimensionvector/
rdfshttp://www.w3.org/2000/01/rdf-schema#
skoshttp://www.w3.org/2004/02/skos/core#
n8http://qudt.org/2.1/vocab/
rdfhttp://www.w3.org/1999/02/22-rdf-syntax-ns#
xsdhhttp://www.w3.org/2001/XMLSchema#

Statements

Subject Item
n2:FLIGHT-PERFORMANCE-RESERVE-PROPELLANT-MASS
rdf:type
n3:QuantityKind
rdfs:label
Flight Performance Reserve Propellant Mass
rdfs:isDefinedBy
n8:quantitykind
skos:broader
n2:Mass
skos:altLabel
FPR
n3:applicableUnit
n4:CWT_LONG n4:Stone_UK n4:SolarMass n4:OZ n4:DecaGM n4:CARAT n4:PlanckMass n4:SLUG n4:LB n4:AMU n4:U n4:TONNE n4:FemtoGM n4:TON_SHORT n4:TON_UK n4:EarthMass n4:TON_US n4:DRAM_UK n4:KiloGM n4:TON_Assay n4:NanoGM n4:GM n4:KiloTON_Metric n4:Hundredweight_UK n4:TON_Metric n4:Hundredweight_US n4:DRAM_US n4:TON_LONG n4:KiloTONNE n4:DWT n4:LunarMass n4:DeciTON_Metric n4:GRAIN n4:Quarter_UK n4:DeciTONNE n4:CentiGM n4:PicoGM n4:MegaGM n4:HectoGM n4:MilliGM n4:MicroGM n4:LB_T n4:OZ_TROY n4:Pennyweight n4:CWT_SHORT n4:DeciGM
n3:hasDimensionVector
n6:A0E0L0I0M1H0T0D0
n3:plainTextDescription
A quantity of propellant, at a nominal mixture ratio, along with fuel bias that is set aside from total propellant loaded to cover for statistical variations of flight hardware characteristics and environment conditions on the day of launch. The launch vehicle is designed to accommodate the maximum FPR loading.