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Reduced mass and Specific orbital energy

Shortcuts: Differences, Similarities, Jaccard Similarity Coefficient, References.

Difference between Reduced mass and Specific orbital energy

Reduced mass vs. Specific orbital energy

In physics, the reduced mass is the "effective" inertial mass appearing in the two-body problem of Newtonian mechanics. In the gravitational two-body problem, the specific orbital energy \epsilon\,\! (or vis-viva energy) of two orbiting bodies is the constant sum of their mutual potential energy (\epsilon_p\,\!) and their total kinetic energy (\epsilon_k\,\!), divided by the reduced mass.

Similarities between Reduced mass and Specific orbital energy

Reduced mass and Specific orbital energy have 1 thing in common (in Unionpedia): Standard gravitational parameter.

Standard gravitational parameter

In celestial mechanics, the standard gravitational parameter μ of a celestial body is the product of the gravitational constant G and the mass M of the body.

Reduced mass and Standard gravitational parameter · Specific orbital energy and Standard gravitational parameter · See more »

The list above answers the following questions

Reduced mass and Specific orbital energy Comparison

Reduced mass has 25 relations, while Specific orbital energy has 30. As they have in common 1, the Jaccard index is 1.82% = 1 / (25 + 30).

References

This article shows the relationship between Reduced mass and Specific orbital energy. To access each article from which the information was extracted, please visit:

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