Trev
The Dumb One
Just seen this bit about using a satellite to 'sweep up' space junk.
They said that bits of junk can hit other satellites at velocities of up to 27,000 MPH.
As the junk is likely to be in substantially the same low earth orbit (LEO) as the 'wanted' sat, how can the closing velocity be that high when the velocity for LEO is around 17,500 MPH. I suppose that this relative velocity could be achieved by the approach of a polar(ish) orbiting object to and equatorial(ish) orbiting object? Otherwise it would require that one object is orbiting 'the other way round'.
Presumably, as there is likely to be more junk in equatorial(ish) (as opposed to polar(ish) orbits, this is what they will 'go for' first.
The animation showed the 'collector' orbiting a short distance from the 'debris' at a similar velocity so unless the 'collector' satellite itself presents a 27,000 MPH closing velocity hazard to collect the 27,000 MPH junk, how does it all work?
They said that bits of junk can hit other satellites at velocities of up to 27,000 MPH.
As the junk is likely to be in substantially the same low earth orbit (LEO) as the 'wanted' sat, how can the closing velocity be that high when the velocity for LEO is around 17,500 MPH. I suppose that this relative velocity could be achieved by the approach of a polar(ish) orbiting object to and equatorial(ish) orbiting object? Otherwise it would require that one object is orbiting 'the other way round'.
Presumably, as there is likely to be more junk in equatorial(ish) (as opposed to polar(ish) orbits, this is what they will 'go for' first.
The animation showed the 'collector' orbiting a short distance from the 'debris' at a similar velocity so unless the 'collector' satellite itself presents a 27,000 MPH closing velocity hazard to collect the 27,000 MPH junk, how does it all work?