All future satellites launched should have a deorbit capacity. This capacity needs to be autonomous of the satellite itself. Obviously weight is a premium but that is getting more and more mitigated with things like spacex.
Is there a way to distinguish the scenarios by the amount of debris and measurable characteristics such the delta v of the debris relative to the original satellite.
Gee, could you be more stiff?
All future satellites launched should have a deorbit capacity. This capacity needs to be autonomous of the satellite itself. Obviously weight is a premium but that is getting more and more mitigated with things like spacex.
Is there a way to distinguish the scenarios by the amount of debris and measurable characteristics such the delta v of the debris relative to the original satellite.