Free-fall time

The free-fall time is the characteristic time that would take a body to collapse under its own gravitational attraction, if no other forces existed to oppose the collapse. As such, it plays a fundamental role in setting the timescale for a wide variety of astrophysical processes—from star formation to helioseismology to supernovae—in which gravity plays a dominant role. The free-fall time is the characteristic time that would take a body to collapse under its own gravitational attraction, if no other forces existed to oppose the collapse. As such, it plays a fundamental role in setting the timescale for a wide variety of astrophysical processes—from star formation to helioseismology to supernovae—in which gravity plays a dominant role. It is relatively simple to derive the free-fall time by applying nothing more than Kepler's Third Law of planetary motion to a degenerate elliptic orbit. Consider a point mass m {displaystyle m} at distance R {displaystyle R} from a point source of mass M {displaystyle M} which falls radially inward to it. Crucially, Kepler's Third Law depends only on the semi-major axis of the orbit, and does not depend on the eccentricity. A purely radial trajectory is an example of a degenerate ellipse with an eccentricity of 1 and semi-major axis R / 2 {displaystyle R/2} . Therefore, the time it would take a body to fall inward, turn around, and return to its original position is the same as the period of a circular orbit of radius R / 2 {displaystyle R/2} , or To see that the semi-major axis is R / 2 {displaystyle R/2} , we must examine properties of orbits as they become increasingly elliptical. Kepler's First Law states that an orbit is an ellipse with the center of mass as one focus. In the case of a very small mass falling toward a very large mass M {displaystyle M} , the center of mass is within the larger mass. The focus of an ellipse is increasingly off-center with increasing ellipticity. In the limiting case of a degenerate ellipse with an eccentricity of 1, the orbit extends from the initial position of the infalling object ( R {displaystyle R} ) to the point source of mass M {displaystyle M} . In other words, the ellipse becomes a line of length R {displaystyle R} . The semi-major axis is half the width of the ellipse along the long axis, which in the degenerate case becomes R / 2 {displaystyle R/2} . If the free-falling body completed a full orbit, it would begin at distance R {displaystyle R} from the point source mass M {displaystyle M} , fall inward until it reached that point source, then turn around and journey back to its original position. In real systems, the point source mass isn't truly a point source and the infalling body eventually collides with some surface. Thus, it only completes half the orbit. But since the infalling part of the orbit is symmetric to the hypothetical outgoing portion of the orbit, we can simply divide the period of the full orbit by two to attain the free-fall time (the time along the infalling portion of the orbit). This formula also follows from the formula for the falling time as a function of position. Note that t orbit {displaystyle t_{ ext{orbit}}} in the above equation, is the time for the mass to fall in a highly eccentric orbit, make a 'hairpin' turn at the central mass at nearly zero radius distance, and then returns to R when it repeats the very sharp turn. This orbit corresponds to nearly linear motion back and from distance R to distance 0. As noted above, this orbit has only half as long a semimajor axis (R/2) as a circular orbit with radius R (where the semimajor axis is R), and thus the period for the shorter high-eccentricity 'orbit' is that for one with an axis of R/2 and a total orbital pathlength of only twice the infall distance. Thus, by Kepler's third law, with half the semimajor axis radius it thus takes only (1/2)3/2 = (1/8)1/2 as long a time period, as the 'corresponding' circular orbit that has a constant radius the same as the maximal radius of the eccentric orbit (which goes to essentially zero radius from the primary at its other extreme). The time to traverse half the distance R, which is the infall time from R along an eccentric orbit, is the Kepler time for a circular orbit of R/2 (not R), which is (1/32)1/2 times the period P of the circular orbit at R. For example, the time for an object in the orbit of the Earth around the Sun, to fall into the Sun if it were suddenly stopped in orbit, would be P / 32 {displaystyle P/{sqrt {32}}} , where P is one year. This is about 64.6 days. Now, consider a case where the mass M {displaystyle M} is not a point mass, but is distributed in a spherically-symmetric distribution about the center, with an average mass density of ρ {displaystyle ho } , where the volume of a sphere is: ( 4 / 3 ) π R 3 . {displaystyle {(4/3)pi R^{3}}.}