J. Ashenberg, FORMULAS FOR THE PHASE CHARACTERISTICS IN THE PROBLEM OF LOW EARTH ORBITAL DEBRIS, Journal of spacecraft and rockets, 31(6), 1994, pp. 1044-1049
Some formulas and relations for estimating the characteristics of the
different phases in the problem of debris propagation are suggested. T
he methods are based on the assumption of a weak isotropic explosion a
s the orbital breakup mechanism. This assumption leads to a simple for
mulation of the torus, the apsidal, and the nodal closure times. A cri
terion that guarantees the separation of the atmospheric dissipation p
hase from the nodal dispersion is suggested as well.