Standard gravitational parameter
|Body||μ (m3 s−2)|
For several objects in the Solar System, the value of μ is known to greater accuracy than either G or M. The SI units of the standard gravitational parameter are m3 s−2. However, units of km3 s−2 are frequently used in the scientific literature and in spacecraft navigation.
Small body orbiting a central bodyEdit
The central body in an orbital system can be defined as the one whose mass (M) is much larger than the mass of the orbiting body (m), or M ≫ m. This approximation is standard for planets orbiting the Sun or most moons and greatly simplifies equations. Under Newton's law of universal gravitation, if the distance between the bodies is r, the force exerted on the smaller body is:
Thus only the product of G and M is needed to predict the motion of the smaller body. Conversely, measurements of the smaller body's orbit only provide information on the product, μ, not G and M separately. The gravitational constant, G, is difficult to measure with high accuracy, while orbits, at least in the solar system, can be measured with great precision and used to determine μ with similar precision.
For a circular orbit around a central body:
This can be generalized for elliptic orbits:
Two bodies orbiting each otherEdit
In the more general case where the bodies need not be a large one and a small one (the two-body problem), we define:
- the vector r is the position of one body relative to the other
- r, v, and in the case of an elliptic orbit, the semi-major axis a, are defined accordingly (hence r is the distance)
- μ = Gm1 + Gm2 = μ1 + μ2, where m1 and m2 are the masses of the two bodies.
- for circular orbits, rv2 = r3ω2 = 4π2r3/T2 = μ
- for elliptic orbits, 4π2a3/T2 = μ (with a expressed in AU; T in seconds and M the total mass relative to that of the Sun, we get a3/T2 = M)
- for parabolic trajectories, rv2 is constant and equal to 2μ
- for elliptic and hyperbolic orbits, μ is twice the semi-major axis times the absolute value of the specific orbital energy, where the latter is defined as the total energy of the system divided by the reduced mass.
Terminology and accuracyEdit
The value for the Earth is called the geocentric gravitational constant and equals 004418±0.000000008)×1014 m3 s−2. (3.986 The uncertainty is just 1 to 000000 because this quantity is derived from the movement of artificial satellites, which basically involves observations of the distances from the satellite to earth stations at different times, which can be obtained to high accuracy using radar or laser ranging. 500
However, the M (mass of the Earth in kilograms) can be found out only by dividing the MG by G, and the G is known only by laboratory measures of the attraction between two known masses. The uncertainty of those measures is 1 to , so M will have the same uncertainty. 7000
The value for the Sun is called the heliocentric gravitational constant or geopotential of the Sun and equals 12440042±0.0000000001)×1020 m3 s−2. (1.327 The uncertainty in the HGC is smaller than the uncertainty in the GGC because the HGC is derived from the ranging of interplanetary probes, and the absolute error of the distance measures to them is about the same as the earth satellite ranging measures, while the absolute distances involved are much bigger.
Note that the reduced mass is also denoted by μ.
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