About: Specific Impulse

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An Entity of Type : http://qudt.org/schema/qudt/QuantityKind, within Data Space : foodie-cloud.org, foodie-cloud.org associated with source document(s)

Attributes	Values
type	Quantity Kind
label	Specific Impulse (en)
isDefinedBy	QUDT Quantity Kind Vocabulary Version 2.1.29
seeAlso	Mass Flow Rate
Description	The impulse produced by a rocket divided by the mass \(mp\) of propellant consumed. Specific impulse \({I_{sp}}\) is a widely used measure of performance for chemical, nuclear, and electric rockets. It is usually given in seconds for both U.S. Customary and International System (SI) units. The impulse produced by a rocket is the thrust force \(F\) times its duration \(t\) in seconds. \(I_{sp}\) is the thrust per unit mass flowrate, but with \(g_o\), is the thrust per weight flowrate. The specific impulse is given by the equation: \(I_{sp} = \frac{F}{\dot{m}g_o}\). (http://qudt.org/schema/qudt/LatexString)
http://qudt.org/sc...asDimensionVector	http://qudt.org/vocab/dimensionvector/A0E0L0I0M0H0T1D0
http://qudt.org/sc...ormativeReference	http://www.grc.nasa.gov/WWW/K-12/airplane/specimp.html
is seeAlso of	Mass Flow Rate Specific thrust
is has broader of	Average Specific Impulse Specific Impulse by Weight

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