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This article is about the distance within which an orbiting object will form rings. For the limits at which an orbiting object will be captured, see Roche lobe. For the gravitational sphere of influence of one astronomical body in the face of perturbations from another heavier body around which it orbits, see Roche sphere.

The **Roche limit** (pronounced /ʁoʃ/ in IPA, similar to the sound of *rosh*), sometimes referred to as the **Roche radius**, is the distance within which a celestial body, held together only by its own gravity, will disintegrate due to a second celestial body's tidal forces exceeding the first body's gravitational self-attraction.^{[1]} Inside the Roche limit, orbiting material disperses and forms rings whereas outside the limit material tends to coalesce. The term is named after Édouard Roche, who is the French astronomer who first calculated this theoretical limit in 1848.^{[2]}

Typically, the Roche limit applies to a satellite's disintegrating due to tidal forces induced by its *primary*, the body about which it orbits. Parts of the satellite that are closer to the primary are attracted by stronger gravity from the primary, whereas parts farther away are repelled by stronger centrifugal force from the satellite's curved orbit. Some real satellites, both natural and artificial, can orbit within their Roche limits because they are held together by forces other than gravitation. Jupiter's moon Metis and Saturn's moon Pan are examples of such satellites, which hold together because of their tensile strength (that is, they are solid and not easily pulled apart). In principle, objects resting on the surface of such a satellite would actually be lifted away by tidal forces. A weaker satellite, such as a comet, could be broken up when it passes within its Roche limit.

Since tidal forces overwhelm the gravity that might hold the satellite together within the Roche limit, no large satellite can gravitationally coalesce out of smaller particles within that limit. Indeed, almost all known planetary rings are located within their Roche limit, Saturn's E-Ring and Phoebe ring being notable exceptions. They could either be remnants from the planet's proto-planetary accretion disc that failed to coalesce into moonlets, or conversely have formed when a moon passed within its Roche limit and broke apart.

The Roche limit is not the only factor that causes comets to break apart. Splitting by thermal stress, internal gas pressure and rotational splitting are other ways for a comet to split under stress.

The limiting distance to which a satellite can approach without breaking up depends on the rigidity of the satellite. At one extreme, a completely rigid satellite will maintain its shape until tidal forces break it apart. At the other extreme, a highly fluid satellite gradually deforms leading to increased tidal forces, causing the satellite to elongate, further compounding the tidal forces and causing it to break apart more readily. Most real satellites would lie somewhere between these two extremes, with tensile strength rendering the satellite neither perfectly rigid nor perfectly fluid. The Roche limit is also usually calculated for the case of a circular orbit, although it is straightforward to modify the calculation to apply to the case (for example) of a body passing the primary on a parabolic or hyperbolic trajectory.

The *rigid-body* Roche limit is a simplified calculation for a spherical satellite. Irregular shapes such as those of tidal deformation on the body or the primary it orbits are neglected. It is assumed to be in hydrostatic equilibrium. These assumptions, although unrealistic, greatly simplify calculations.

The Roche limit for a rigid spherical satellite is the distance, , from the primary at which the gravitational force on a test mass at the surface of the object is exactly equal to the tidal force pulling the mass away from the object:^{[3]}^{[4]}

where is the radius of the primary, is the density of the primary, and is the density of the satellite. This can be equivalently written as

where is the radius of the secondary, is the mass of the primary, and is the mass of the secondary.

This does not depend on the size of the objects, but on the ratio of densities. This is the orbital distance inside of which loose material (e.g. regolith) on the surface of the satellite closest to the primary would be pulled away, and likewise material on the side opposite the primary will also be pulled away from, rather than toward, the satellite.

In order to determine the Roche limit, we consider a small mass on the surface of the satellite closest to the primary. There are two forces on this mass : the gravitational pull towards the satellite and the gravitational pull towards the primary. Assuming that the satellite is in free fall around the primary and that the tidal force is the only relevant term of the gravitational attraction of the primary. This assumption is a simplification as free-fall only truly applies to the planetary center, but will suffice for this derivation.^{[5]}

The gravitational pull on the mass towards the satellite with mass and radius can be expressed according to Newton's law of gravitation.

the tidal force on the mass towards the primary with radius and mass , at a distance between the centers of the two bodies, can be expressed approximately as

- .

To obtain this approximation, find the difference in the primary's gravitational pull on the center of the satellite and on the edge of the satellite closest to the primary:

In the approximation where r<<R and R<d, we can say that the in the numerator and every term with in the denominator goes to zero, which gives us:

The Roche limit is reached when the gravitational force and the tidal force balance each other out.

or

- ,

which gives the Roche limit, , as

- .

However, we don't really want the radius of the satellite to appear in the expression for the limit, so we re-write this in terms of densities.

For a sphere the mass can be written as

- where is the radius of the primary.

And likewise

- where is the radius of the satellite.

Substituting for the masses in the equation for the Roche limit, and cancelling out gives

- ,

which can be simplified to the Roche limit:

- .

Since a close satellite will likely be orbiting in a nearly-circular orbit with synchronous rotation, let us consider how the centrifugal force from rotation will affect the results. That force is

and it gets added to F_{T}. Doing the force-balance calculation yields this result for the Roche limit:

- .

A more accurate approach for calculating the Roche limit takes the deformation of the satellite into account. An extreme example would be a tidally locked liquid satellite orbiting a planet, where any force acting upon the satellite would deform it into a prolate spheroid.

The calculation is complex and its result cannot be represented in an exact algebraic formula. Roche himself derived the following approximate solution for the Roche limit:

However, a better approximation that takes into account the primary's oblateness and the satellite's mass is:

where is the oblateness of the primary. The numerical factor is calculated with the aid of a computer.

The fluid solution is appropriate for bodies that are only loosely held together, such as a comet. For instance, comet Shoemaker–Levy 9's decaying orbit around Jupiter passed within its Roche limit in July 1992, causing it to fragment into a number of smaller pieces. On its next approach in 1994 the fragments crashed into the planet. Shoemaker–Levy 9 was first observed in 1993, but its orbit indicated that it had been captured by Jupiter a few decades prior.^{[6]}

As the fluid satellite case is more delicate than the rigid one, the satellite is described with some simplifying assumptions. First, assume the object consists of incompressible fluid that has constant density and volume that do not depend on external or internal forces.

Second, assume the satellite moves in a circular orbit and it remains in synchronous rotation. This means that the angular speed at which it rotates around its center of mass is the same as the angular speed at which it moves around the overall system barycenter.

The angular speed is given by Kepler's third law:

When M is very much bigger than m, this will be close to

The synchronous rotation implies that the liquid does not move and the problem can be regarded as a static one. Therefore, the viscosity and friction of the liquid in this model do not play a role, since these quantities would play a role only for a moving fluid.

Given these assumptions, the following forces should be taken into account:

- The force of gravitation due to the main body;
- the centrifugal force in the rotary reference system; and
- the self-gravitation field of the satellite.

Since all of these forces are conservative, they can be expressed by means of a potential. Moreover, the surface of the satellite is an equipotential one. Otherwise, the differences of potential would give rise to forces and movement of some parts of the liquid at the surface, which contradicts the static model assumption. Given the distance from the main body, our problem is to determine the form of the surface that satisfies the equipotential condition.

As the orbit has been assumed circular, the total gravitational force and orbital centrifugal force acting on the main body cancel. That leaves two forces: the tidal force and the rotational centrifugal force. The tidal force depends on the position with respect to the center of mass, already considered in the rigid model. For small bodies, the distance of the liquid particles from the center of the body is small in relation to the distance *d* to the main body. Thus the tidal force can be linearized, resulting in the same formula for *F _{T}* as given above.

While this force in the rigid model depends only on the radius *r* of the satellite, in the fluid case we need to consider all the points on the surface and the tidal force depends on the distance *Δd* from the center of mass to a given particle projected on the line joining the satellite and the main body. We call *Δd* the *radial distance*. Since the tidal force is linear in *Δd*, the related potential is proportional to the square of the variable and for we have

Likewise, the centrifugal force has a potential

for rotational angular velocity .

We want to determine the shape of the satellite for which the sum of the self-gravitation potential and *V _{T} + V_{C}* is constant on the surface of the body. In general, such a problem is very difficult to solve, but in this particular case, it can be solved by a skillful guess due to the square dependence of the tidal potential on the radial distance

Since the potential *V _{T}* changes only in one direction,

where is the constant self-potential on the intersection of the circular edge of the body and the central symmetry plane given by the equation *Δd=0*.

The dimensionless function *f* is to be determined from the accurate solution for the potential of the ellipsoid

and, surprisingly enough, does not depend on the volume of the satellite.

Although the explicit form of the function *f* looks complicated, it is clear that we may and do choose the value of *ε* so that the potential *V _{T}* is equal to

This equation can be solved numerically. The graph indicates that there are two solutions and thus the smaller one represents the stable equilibrium form (the ellipsoid with the smaller eccentricity). This solution determines the eccentricity of the tidal ellipsoid as a function of the distance to the main body. The derivative of the function *f* has a zero where the maximal eccentricity is attained. This corresponds to the Roche limit.

More precisely, the Roche limit is determined by the fact that the function *f*, which can be regarded as a nonlinear measure of the force squeezing the ellipsoid towards a spherical shape, is bounded so that there is an eccentricity at which this contracting force becomes maximal. Since the tidal force increases when the satellite approaches the main body, it is clear that there is a critical distance at which the ellipsoid is torn up.

The maximal eccentricity can be calculated numerically as the zero of the derivative of *f'*. One obtains

which corresponds to the ratio of the ellipsoid axes 1:1.95. Inserting this into the formula for the function *f* one can determine the minimal distance at which the ellipsoid exists. This is the Roche limit,

Surprisingly, including the centrifugal potential makes remarkably little difference, though the object becomes a *Roche ellipsoid*, a general triaxial ellipsoid with all axes having different lengths. The potential becomes a much more complicated function of the axis lengths, requiring elliptic functions. However, the solution proceeds much as in the tidal-only case, and we find

The ratios of polar to orbit-direction to primary-direction axes are 1:1.06:2.07.

This section may be too technical for most readers to understand. (March 2014) |

The table below shows the mean density and the equatorial radius for selected objects in the Solar System.

Primary | Density (kg/m^{3}) | Radius (m) |
---|---|---|

Sun | 1,408 | 696,000,000 |

Jupiter | 1,326 | 71,492,000 |

Earth | 5,513 | 6,378,137 |

Moon | 3,346 | 1,738,100 |

Saturn | 687 | 60,268,000 |

Uranus | 1,318 | 25,559,000 |

Neptune | 1,638 | 24,764,000 |

Using these data, the Roche limits for rigid and fluid bodies can be calculated. The average density of comets is taken to be around 500 kg/m³.

The table below gives the Roche limits expressed in kilometres and in primary radii. The true Roche limit for a satellite depends on its density and rigidity.

Body | Satellite | Roche limit (rigid) | Roche limit (fluid) | ||
---|---|---|---|---|---|

Distance (km) | R | Distance (km) | R | ||

Earth | Moon | 9,496 | 1.49 | 18,261 | 2.86 |

Earth | average comet | 17,880 | 2.80 | 34,390 | 5.39 |

Sun | Earth | 554,400 | 0.80 | 1,066,300 | 1.53 |

Sun | Jupiter | 890,700 | 1.28 | 1,713,000 | 2.46 |

Sun | Moon | 655,300 | 0.94 | 1,260,300 | 1.81 |

Sun | average comet | 1,234,000 | 1.78 | 2,374,000 | 3.42 |

How close are the Solar System's moons to their Roche limits? The table below gives each inner satellite's orbital radius divided by its own Roche radius. Both rigid and fluid body calculations are given. Note that Pan, Cordelia and Naiad, in particular, may be quite close to their actual break-up points.

In practice, the densities of most of the inner satellites of giant planets are not known. In these cases, shown in *italics*, likely values have been assumed, but their *actual* Roche limit can vary from the value shown.

Primary | Satellite | Orbital Radius / Roche limit | |
---|---|---|---|

(rigid) | (fluid) | ||

Sun | Mercury | 104:1 | 54:1 |

Earth | Moon | 41:1 | 21:1 |

Mars | Phobos | 172% | 89% |

Deimos | 451% | 234% | |

Jupiter | Metis | ~186% | ~94% |

Adrastea | ~188% | ~95% | |

Amalthea | 175% | 88% | |

Thebe | 254% | 128% | |

Saturn | Pan | 142% | 70% |

Atlas | 156% | 78% | |

Prometheus | 162% | 80% | |

Pandora | 167% | 83% | |

Epimetheus | 200% | 99% | |

Janus | 195% | 97% | |

Uranus | Cordelia | ~154% | ~79% |

Ophelia | ~166% | ~86% | |

Bianca | ~183% | ~94% | |

Cressida | ~191% | ~98% | |

Desdemona | ~194% | ~100% | |

Juliet | ~199% | ~102% | |

Neptune | Naiad | ~139% | ~72% |

Thalassa | ~145% | ~75% | |

Despina | ~152% | ~78% | |

Galatea | 153% | 79% | |

Larissa | ~218% | ~113% | |

Pluto | Charon | 12.5:1 | 6.5:1 |

- Roche lobe
- Chandrasekhar limit
- Hill sphere
- Spaghettification (a rather extreme tidal distortion)
- Black hole
- Triton (moon) (Neptune satellite)
- Comet Shoemaker–Levy 9

**^**Eric W. Weisstein (2007). "Eric Weisstein's World of Physics – Roche Limit". scienceworld.wolfram.com. Retrieved September 5, 2007.**^**NASA. "What is the Roche limit?". NASA – JPL. Retrieved September 5, 2007.**^**see calculation in Frank H. Shu,*The Physical Universe: an Introduction to Astronomy,*p. 431, University Science Books (1982), ISBN 0-935702-05-9.**^**"Roche Limit: Why Do Comets Break Up?".**^**Gu et al. "The effect of tidal inflation instability on the mass and dynamical evolution of extrasolar planets with ultrashort periods". Astrophysical Journal. Retrieved May 1, 2003.**^**International Planetarium Society Conference, Astronaut Memorial Planetarium & Observatory, Cocoa, Florida Rob Landis 10–16 July 1994 archive 21/12/1996

- Édouard Roche: "La figure d'une masse fluide soumise à l'attraction d'un point éloigné" (The figure of a fluid mass subjected to the attraction of a distant point), part 1,
*Académie des sciences de Montpellier: Mémoires de la section des sciences*, Volume 1 (1849) 243–262. 2.44 is mentioned on page 258. (French) - Édouard Roche: "La figure d'une masse fluide soumise à l'attraction d'un point éloigné", part 2,
*Académie des sciences de Montpellier: Mémoires de la section des sciences*, Volume 1 (1850) 333–348. (French) - Édouard Roche: "La figure d'une masse fluide soumise à l'attraction d'un point éloigné", part 3,
*Académie des sciences de Montpellier: Mémoires de la section des sciences*, Volume 2 (1851) 21–32. (French) - George Howard Darwin, "On the figure and stability of a liquid satellite",
*Scientific Papers, Volume 3*(1910) 436–524. - James Hopwood Jeans,
*Problems of cosmogony and stellar dynamics*, Chapter III: Ellipsoidal configurations of equilibrium, 1919. - S. Chandrasekhar,
*Ellipsoidal figures of equilibrium*(New Haven: Yale University Press, 1969), Chapter 8: The Roche ellipsoids (189–240). - S. Chandrasekhar, "The equilibrium and the stability of the Roche ellipsoids",
*Astrophysical Journal*138 (1963) 1182–1213.

- Discussion of the Roche Limit
- Audio: Cain/Gay – Astronomy Cast Tidal Forces Across the Universe – July 2007. Cập nhật 6/8/2007