Engineering analysis demonstrates pneumatic encapsulation accelerates orbital decay to under two decades for heavy derelict rocket stages, indicating a scalable multi-target remediation approach.
Abstract (da incollare nel campo Description) Active Debris Removal (ADR) programs in Low Earth Orbit (LEO) are historically constrained by the prohibitive operational cost of the conventional 1-to-1 retrieval model, where an interceptor vehicle expends extensive propellant to capture and de-orbit a single derelict target before being discarded. In this paper, we propose the Multi-Target Encapsulation Architecture (MTEA), a nautical-inspired, passive remediation paradigm. Instead of hunting distributed micro-fragments or relying on active propulsive descent, MTEA deploys an autonomous hybrid-propulsion tug to service multiple massive rocket stages (such as the Soviet SL-16/Zenit-2 cluster at i ≈ 71^∘) in a single campaign. The mechanism utilizes an axial radial-mandrel docked into the main engine nozzle, deploying an oversized, pneumatic multi-layer sleeve based on the principle of a nautical fyke net (nassa). Once cinched and pressurized, the resulting standoff capsule (D ≈ 14 m) provides dual functionality: an omnidirectional, flexible Whipple shield preventing secondary fragmentation from hypervelocity micro-impacts, and an engineered ballistic drag surface. The drastic increase in the Area-to-Mass ratio ($A/m$) exploits residual thermospheric friction to reduce passive orbital decay timelines from centuries to less than two decades. The mission design, aerodynamic passivity, megaconstellation transit safety, and a multilateral consortium economic model are systematically formulated.
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ROCCA et al. (2026) studied this question.
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