Abstract

This white paper establishes a deterministic framework for regulating Low Earth Orbit (LEO) mass allocations. It defines the physical boundaries of orbital sustainability against three core degradation vectors: stratospheric chemical ablation, kinetic debris cascades, and optical astronomy occlusion. By translating raw physical constraints into closed-form regulatory mechanisms, this document provides the mathematical foundation necessary to move global aerospace policy from permissive liability models to definitive, thermodynamic carrying-capacity caps.

Creative Commons License

Creative Commons License
This work is licensed under a Creative Commons Attribution 4.0 License.

379 - A.pdf (41 kB)
LaTeX

379 - B.pdf (45 kB)
SPEC-379-CORE: Kessler Matrix Stability & Eigenvalue Tracker Evaluates Low Earth Orbit (LEO) populations for catastrophic tipping points

379 - C.pdf (43 kB)
APPENDIX C: EMPIRICAL DATA MATRIX

379 - D.pdf (87 kB)
APPENDIX D: MATHEMATICAL PROOF OF THE LAMBERTIAN PHASE FUNCTION \(q(\psi)\)

380 - Taxonomy.pdf (101 kB)
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