The main objective of this thesis is to find the best way to deorbit spent spacecrafts and upper stages. Deorbit has been proven to be the most effective measure for long term space debris mitigation. The analysis will focus on LEO orbital region, that is the most populated region of space, and consequently the region where implementation of deorbit is most necessary and urgent. Several solutions proposed in literature as deorbit systems will be analyzed and compared, based on numerical data
Debris Mitigation in LEO Orbits: Performance Analysis and Comparison of different Deorbit Systems
Pastore, Guido
2014/2015
Abstract
The main objective of this thesis is to find the best way to deorbit spent spacecrafts and upper stages. Deorbit has been proven to be the most effective measure for long term space debris mitigation. The analysis will focus on LEO orbital region, that is the most populated region of space, and consequently the region where implementation of deorbit is most necessary and urgent. Several solutions proposed in literature as deorbit systems will be analyzed and compared, based on numerical dataFile in questo prodotto:
| File | Dimensione | Formato | |
|---|---|---|---|
|
THESIS_LAUREA_MAGISTRALE_-_Pastore_Guido.pdf
accesso aperto
Dimensione
6.11 MB
Formato
Adobe PDF
|
6.11 MB | Adobe PDF | Visualizza/Apri |
The text of this website © Università degli studi di Padova. Full Text are published under a non-exclusive license. Metadata are under a CC0 License
Utilizza questo identificativo per citare o creare un link a questo documento:
https://hdl.handle.net/20.500.12608/18620