Reentry trajectories to the Earth have been recently considered as a valuable end-of-life option also for Libration Point Orbits (LPO) missions. In this work, we investigate in detail the case corresponding to SOHO. On the one hand, we show how the main uncertainties associated with the problem affect the probability of reentry and the corresponding point at the interface with the atmosphere. Monte Carlo propagations are applied to different cases of uncertainties. They correspond to the orbit determination, the efficiency of the maneuver required to target the Earth, and the characteristics of the spacecraft determining the solar radiation pressure effect. On the other hand, we provide a comparison between a classical reentry from a LEO and a hypervelocity reentry from a LPO, in terms of ground casualty area and demise percentage.
On the Reentry Design for the SOHO Mission
Alessi EM;
2017
Abstract
Reentry trajectories to the Earth have been recently considered as a valuable end-of-life option also for Libration Point Orbits (LPO) missions. In this work, we investigate in detail the case corresponding to SOHO. On the one hand, we show how the main uncertainties associated with the problem affect the probability of reentry and the corresponding point at the interface with the atmosphere. Monte Carlo propagations are applied to different cases of uncertainties. They correspond to the orbit determination, the efficiency of the maneuver required to target the Earth, and the characteristics of the spacecraft determining the solar radiation pressure effect. On the other hand, we provide a comparison between a classical reentry from a LEO and a hypervelocity reentry from a LPO, in terms of ground casualty area and demise percentage.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
