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View article: The space environment particle density in Low Earth Orbit based on two decades of in-situ observation
The space environment particle density in Low Earth Orbit based on two decades of in-situ observation Open
Currently the only method to establish the prevalence of particles, space debris or meteoroids, sized between 1 micrometre and a few centimetres, in Earth orbit is by instruments or witness plates dedicated to in-situ detection. Derived us…
View article: Density-based evolutionary model of the space debris environment in low-Earth orbit
Density-based evolutionary model of the space debris environment in low-Earth orbit Open
View article: Analysis of accidental spacecraft break-up events in cislunar space
Analysis of accidental spacecraft break-up events in cislunar space Open
View article: Medium-term Predictions of F10.7 and F30 cm Solar Radio Flux with the Adaptive Kalman Filter
Medium-term Predictions of F10.7 and F30 cm Solar Radio Flux with the Adaptive Kalman Filter Open
The solar radio flux at F10.7 and F30 cm is required by most models characterizing the state of the Earth’s upper atmosphere, such as the thermosphere and ionosphere, to specify satellite orbits, re-entry services, collision avoidance mane…
View article: Design of a Software to Assess the Impact of a Space Mission on the Space Environment
Design of a Software to Assess the Impact of a Space Mission on the Space Environment Open
View article: Application of Density-Based Propagation to Fragment Clouds Using the Starling Suite
Application of Density-Based Propagation to Fragment Clouds Using the Starling Suite Open
View article: Extension of the King-Hele orbit contraction method for accurate, semi-analytical propagation of non-circular orbits
Extension of the King-Hele orbit contraction method for accurate, semi-analytical propagation of non-circular orbits Open
View article: Interpolation and Integration of Phase Space Density for Estimation of Fragmentation Cloud Distribution
Interpolation and Integration of Phase Space Density for Estimation of Fragmentation Cloud Distribution Open
To calculate the effects of on-orbit fragmentations on current or future space missions, accurate estimates of the fragment density and its time evolution are required. Current operational tools estimate the risks involved through represen…
View article: Radar-based Re-Entry Predictions with very limited tracking\n capabilities: the GOCE case study
Radar-based Re-Entry Predictions with very limited tracking\n capabilities: the GOCE case study Open
The problem of the re-entry predictions of GOCE has been deeply investigated\nin the literature, due to the large amount of data, mainly radar and GPS,\navailable until re-entry. The accurate GPS and attitude measurements are used\nto comp…
View article: Radar-based Re-Entry Predictions with very limited tracking capabilities: the GOCE case study
Radar-based Re-Entry Predictions with very limited tracking capabilities: the GOCE case study Open
The problem of the re-entry predictions of GOCE has been deeply investigated in the literature, due to the large amount of data, mainly radar and GPS, available until re-entry. The accurate GPS and attitude measurements are used to compute…
View article: The observing campaign on the deep-space debris WT1190F as a test case for short-warning NEO impacts
The observing campaign on the deep-space debris WT1190F as a test case for short-warning NEO impacts Open
View article: Impact of End-of-Life manoeuvres on the collision risk in protected regions
Impact of End-of-Life manoeuvres on the collision risk in protected regions Open
View article: Life Cycle Assessment Indicator for Space Debris
Life Cycle Assessment Indicator for Space Debris Open
In the framework of space debris remediation and mitigation and eco-design of space systems, a design indicator is proposed to measure the management of
end-of-life options and to compare different design options of a space mission fro…
end-of-life options and to compare different design options of a space mission fro…
View article: Evolution of Fragmentation Cloud in Highly Eccentric Orbit Using Representative Objects
Evolution of Fragmentation Cloud in Highly Eccentric Orbit Using Representative Objects Open
Many historical on-orbit satellite fragmentations occurred in Highly Eccentric Orbits (HEOs) such as the Geostationary Transfer Orbit (GTO). Such fragmentations produce fragment clouds that interfere with the Low Earth Orbit (LEO) environm…