Specific Orbital Energy
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High Quality Content by WIKIPEDIA articles! In astrodynamics the specific orbital energy epsilon,! (or vis-viva energy) of an orbiting body traveling through space under standard assumptions is the sum of its potential energy (epsilonp,!) and kinetic energy (epsilonk,!) per unit mass. According to the orbital energy conservation equation (also referred to as vis-viva equation) it is the same at all points of the trajectory: epsilon=epsilonk+epsilonp={v^2over{2}}-{muover{r}} =-{1over{2}}{mu^2over{h^2}}left(1-e^2right) where: v,! is the orbital speed of the orbiting body; r,! is the orbital distance of the orbiting body; mu = GM,! is the standard gravitational parameter of the primary body; h,! is the specific relative angular momentum of the orbiting body; e,! is the orbit eccentricity. It is expressed in J/kg = m²s-2 or MJ/kg = km²s-2.
Weitere Informationen
- Allgemeine Informationen
- GTIN 09786131083044
- Editor Lambert M. Surhone, Miriam T. Timpledon, Susan F. Marseken
- Genre Physik & Astronomie
- EAN 9786131083044
- Format Fachbuch
- Titel Specific Orbital Energy
- Herausgeber Betascript Publishing
- Anzahl Seiten 68
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