A method for creating an artificial reentry corridor. Several modules are deployed in a retrograde orbit relative to target debris. Each module releases a gas plume which, in turn creates an artificial reentry corridor. The debris passes through the corridor and becomes decelerated.
ORBITAL ARTIFICIAL REENTRY CORRIDOR
24.02.2022
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Heeling-angle-availability-based optimal planning method of reentry corridor
Europäisches Patentamt | 2015
|Reentry of Skylab (Orbital Computation Aspect)
NTIS | 1981
|The Reentry of Large Orbital Debris
British Library Conference Proceedings | 1999
|