Self-Amplifying Orbital Recovery Meshes under Multilateral Scrap-Disposal Authority

This paper proposes a two-layer theoretical framework for orbital debris recovery based on Self-Amplifying Orbital Recovery Meshes and Multilateral Scrap-Disposal Authority.

 

Instead of treating space debris only as material to be destroyed through atmospheric re-entry, the framework defines authorized orbital scrap as a temporary functional resource. Under this model, selected debris-derived structures, panels, membranes, reflectors, capture interfaces, and other low-criticality components may be converted into disposable recovery capacity.

 

The proposed system does not rely on full self-replication or high-reliability manufacturing of new spacecraft from debris. Instead, it introduces disposable salvage nodes, capture tags, relay nodes, drag-sail units, containment devices, and use-and-dive recovery elements that expand cleanup capability only within strict limits. These nodes are designed to deorbit even while still operational if their continued presence no longer produces sufficient cleanup value.

 

A central contribution of the paper is the integration of technical recovery logic with a multilateral governance layer. The proposed scrap-disposal authority defines which defunct objects may be approached, captured, partially reused, consumed as disposable recovery tools, sealed, returned, or deorbited. This shifts the legal basis from vague consent to explicit disposal authority.

 

The framework argues that sustainable orbital cleanup requires both controlled technical self-amplification and international authorization for rough disposal. In compact form, the theory can be summarized as follows: authorized debris is converted into temporary recovery capacity; temporary recovery capacity reduces debris; unused recovery capacity removes itself.