We show that for a tether at 800 km altitude, which is 5 km long, 2 cm wide and 0.05 mm thick, the risk of substantial damage during a 3 month period due to multiple impacts with debris or micrometeoroids is low, of about 1.4%. By substantial damage we mean that if the tape is divided in 2 cm2 cm squares, then in some square the damaged area by bombardment with debris or micrometeoroids exceeds 11% of the area of the square. Furthermore, we show that the danger posed by the micrometeoroids is negligible compared to the risk posed by the debris
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...
Various strategies are currently investigated for deorbiting satellites at the end of life to comply...
It has recently been shown that a thin-tape tether, as opposite to a round one, has a high probabili...
The current space environment, consisting of manmade debris and micrometeoroids, poses a risk to saf...
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...
Electrodynamic tethers represent one of the possible means to de-orbit defunct satellites from Low-E...
The materials with vulnerability to micrometeoroids and space debris are discussed. It is concluded ...
A bare tether with thin-tape cross section is both i) the most effective electrodinamic tether for g...
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...
Various strategies are currently investigated for deorbiting satellites at the end of life to comply...
It has recently been shown that a thin-tape tether, as opposite to a round one, has a high probabili...
The current space environment, consisting of manmade debris and micrometeoroids, poses a risk to saf...
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...
Electrodynamic tethers represent one of the possible means to de-orbit defunct satellites from Low-E...
The materials with vulnerability to micrometeoroids and space debris are discussed. It is concluded ...
A bare tether with thin-tape cross section is both i) the most effective electrodinamic tether for g...
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...
Various strategies are currently investigated for deorbiting satellites at the end of life to comply...