The bulge in the Earth at its equator has been shown to lead to a clustering of natural decays biased to occur towards the equator and away from the orbit's extreme latitudes. Such clustering must be considered when predicting the Expectation of Casualty (Ec) during a natural decay, because of the corresponding clustering of the human population in the lower latitudes. This study expands upon prior work, and formalizes in a single empirical equation the correction that must be made to the calculation of the average exposed population density as a result of this effect. The equation is represented as a function of ballistic number and inclination of the entering spacecraft over the credible range of ballistic numbers
Formulas are developed to express the secular acceleration of a satellite on passing through an atmo...
The growth of the population of space debris in the geostationary ring and the resulting threat to a...
A closed form expression for the time to decay between two circular orbit altitudes is developed. Th...
The bulge in the Earth at its equator has been shown to lead to a clustering of natural decays biase...
Prior work has demonstrated pronounced statistical clustering of natural decays of medium-to-high-in...
A number of statistical tools have been developed over the years for assessing the risk of reenterin...
A recent improvement to the long-term estimation of ground casualties from reentering space debris i...
A number of statistical tools have been developed over the years for assessing the risk of reenterin...
Orbital debris experts and industry leaders are concerned about the added hazard that thousands of a...
Historically, computer simulations of the near-Earth space debris environment have provided a basis ...
A consistent methodology for the collation of data from both penetration and perforation experiments...
This project endeavors to find whether it is feasible to use an increase in surface area as a way of...
It is well known that atmospheric density errors are the main source of uncertainty in orbit decay p...
The objective of this paper is to provide a pedagogical framework for the phenomenon of orbital deca...
The geosynchronous orbit (GEO) is a unique commodity of the satellite industry that is becoming incr...
Formulas are developed to express the secular acceleration of a satellite on passing through an atmo...
The growth of the population of space debris in the geostationary ring and the resulting threat to a...
A closed form expression for the time to decay between two circular orbit altitudes is developed. Th...
The bulge in the Earth at its equator has been shown to lead to a clustering of natural decays biase...
Prior work has demonstrated pronounced statistical clustering of natural decays of medium-to-high-in...
A number of statistical tools have been developed over the years for assessing the risk of reenterin...
A recent improvement to the long-term estimation of ground casualties from reentering space debris i...
A number of statistical tools have been developed over the years for assessing the risk of reenterin...
Orbital debris experts and industry leaders are concerned about the added hazard that thousands of a...
Historically, computer simulations of the near-Earth space debris environment have provided a basis ...
A consistent methodology for the collation of data from both penetration and perforation experiments...
This project endeavors to find whether it is feasible to use an increase in surface area as a way of...
It is well known that atmospheric density errors are the main source of uncertainty in orbit decay p...
The objective of this paper is to provide a pedagogical framework for the phenomenon of orbital deca...
The geosynchronous orbit (GEO) is a unique commodity of the satellite industry that is becoming incr...
Formulas are developed to express the secular acceleration of a satellite on passing through an atmo...
The growth of the population of space debris in the geostationary ring and the resulting threat to a...
A closed form expression for the time to decay between two circular orbit altitudes is developed. Th...