| CPC G05D 1/689 (2024.01) [B64G 1/006 (2023.08)] | 30 Claims |

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1. A high-altitude non-destructive aerial object takedown system comprising:
a rocket with a propulsion system;
a takedown payload embedded with the rocket comprising:
a first plurality of ballast units releasable from the takedown payload in a substantially circular capture pattern;
a first plurality of tethers, each tether having a proximal end attached to a corresponding ballast unit and a distal end connected to a takedown payload capture net;
the capture net with a first plurality equally spaced attachment points formed along a capture net perimeter, with each attachment point connected to a corresponding tether; and,
a release mechanism associated with each ballast unit selected from the group consisting of a compressed spring, a gas discharge, and an attached ballast rocket.
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