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Tsiolkovsky rocket equation

The classical rocket equation, Tsiolkovsky rocket equation, or ideal rocket equation is a mathematical equation that describes the motion of vehicles that follow the basic principle of a rocket: a device that can apply acceleration to itself using thrust by expelling part of its mass with high velocity and can thereby move due to the conservation of…

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Tsiolkovsky rocket equation

Nodes71
Edges70
Triples15
Avg. degree1.97
Density0.028169
Components1

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Tsiolkovsky rocket equation

Top relations

related to Mass fraction · 4
Tsiolkovsky rocket equation → Another, In, Tsiolkovsky, While

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Important terminology

mass rocket displaystyle equation propellant velocity delta delta-v text also change total initial frac speed exhaust ln fuel payload derived

Entity relationships Subject–Predicate–Object triples

SubjectPredicateObjectConfidenceSrc
launching frominstance ofis a measure of the impulse that is needed to perform a maneuver0.80text
or landing on a planet or mooninstance ofis a measure of the impulse that is needed to perform a maneuver0.80text
or an in-space orbital maneuverinstance ofis a measure of the impulse that is needed to perform a maneuver0.80text
aerobrakinginstance ofThe equation does not apply to non-rocket systems0.80text
gun launchesinstance ofThe equation does not apply to non-rocket systems0.80text
space elevatorsinstance ofThe equation does not apply to non-rocket systems0.80text
launch loopsinstance ofThe equation does not apply to non-rocket systems0.80text
tether propulsion or light sails.The rocket equation can be applied to orbital maneuvers in order to determine how much propellant is needed to change to a particular new orbitinstance ofThe equation does not apply to non-rocket systems0.80text
or to find the new orbit as the result of a particular propellant burninstance ofThe equation does not apply to non-rocket systems0.80text
for mid-course correctionsinstance ofThis assumption is relatively accurate for short-duration burns0.80text
orbital insertion maneuversinstance ofThis assumption is relatively accurate for short-duration burns0.80text
Tsiolkovsky rocket equationrelated to Mass fractionIn0.60section

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