Tsiolkovsky Rocket Equation
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High Quality Content by WIKIPEDIA articles! The Tsiolkovsky rocket equation, or ideal rocket equation, is a mathematical equation that relates the delta-v with the effective exhaust velocity and the initial and final mass of a rocket. The equation is named after Konstantin Tsiolkovsky who independently derived it and published it in his 1903 work. It considers the principle of a rocket: a device that can apply an acceleration to itself (a thrust) by expelling part of its mass with high speed in the opposite direction, due to the conservation of momentum.
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GarantieWeitere Informationen
- Allgemeine Informationen
- GTIN 09786131155758
- Editor Lambert M. Surhone, Miriam T. Timpledon, Susan F. Marseken
- EAN 9786131155758
- Format Fachbuch
- Titel Tsiolkovsky Rocket Equation
- Herausgeber Betascript Publishing
- Anzahl Seiten 116
- Genre Mathematik
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