The current space environment, consisting of manmade debris and micrometeoroids, poses a risk to safe operations in space, and the situation is continuously deteriorating due to in-orbit debris collisions and to new satellite launches. Bare electrodynamic tethers can provide an efficient mechanism for rapid deorbiting of satellites from low Earth orbit at end of life. Because of its particular geometry (length very much larger than cross-sectional dimensions), a tether may have a relatively high risk of being severed by the single impact of small debris. The rates of fatal impact of orbital debris on round and tape tethers of equal length and mass, evaluated with an analytical approximation to debris flux modeled by NASA’s ORDEM2000, shows ...
De-orbiting satellites at end of mission would prevent generation of new space debris. A proposed de...
De-orbiting satellites at end of mission would prevent generation of new space debris. A proposed de...
International guidelines recommend removing any artificial body in Low Earth Orbit (LEO) within 25 y...
The low earth orbit (LEO) environment contains a large number of artificial debris, of which a signi...
Electrodynamic tethers are a tool to deorbit dead satellites in LEO. These satellites can be shatter...
Electrodynamic tethers are a tool to deorbit dead satellites in LEO. These satellites can be shatter...
There have been a number of proposals for using tethers in space. One such proposal involves deployi...
It has recently been shown that a thin-tape tether, as opposite to a round one, has a high probabili...
We show that for a tether at 800 km altitude, which is 5 km long, 2 cm wide and 0.05 mm thick, the r...
Electrodynamic tethers represent one of the possible means to de-orbit defunct satellites from Low-E...
A bare tether with thin-tape cross section is both i) the most effective electrodinamic tether for g...
De-orbiting satellites at end of mission would prevent generation of new space debris. A proposed de...
The product of the tether-to-satellite mass ratio and the probability of tether cuts by small debri...
De-orbiting satellites at end of mission would prevent generation of new space debris. A proposed de...
De-orbiting satellites at end of mission would prevent generation of new space debris. A proposed de...
De-orbiting satellites at end of mission would prevent generation of new space debris. A proposed de...
De-orbiting satellites at end of mission would prevent generation of new space debris. A proposed de...
International guidelines recommend removing any artificial body in Low Earth Orbit (LEO) within 25 y...
The low earth orbit (LEO) environment contains a large number of artificial debris, of which a signi...
Electrodynamic tethers are a tool to deorbit dead satellites in LEO. These satellites can be shatter...
Electrodynamic tethers are a tool to deorbit dead satellites in LEO. These satellites can be shatter...
There have been a number of proposals for using tethers in space. One such proposal involves deployi...
It has recently been shown that a thin-tape tether, as opposite to a round one, has a high probabili...
We show that for a tether at 800 km altitude, which is 5 km long, 2 cm wide and 0.05 mm thick, the r...
Electrodynamic tethers represent one of the possible means to de-orbit defunct satellites from Low-E...
A bare tether with thin-tape cross section is both i) the most effective electrodinamic tether for g...
De-orbiting satellites at end of mission would prevent generation of new space debris. A proposed de...
The product of the tether-to-satellite mass ratio and the probability of tether cuts by small debri...
De-orbiting satellites at end of mission would prevent generation of new space debris. A proposed de...
De-orbiting satellites at end of mission would prevent generation of new space debris. A proposed de...
De-orbiting satellites at end of mission would prevent generation of new space debris. A proposed de...
De-orbiting satellites at end of mission would prevent generation of new space debris. A proposed de...
International guidelines recommend removing any artificial body in Low Earth Orbit (LEO) within 25 y...