The Orbital Mechanics of Space Elevator Launch Systems
Matthew M. Peet

TL;DR
This paper analyzes the orbital mechanics of space elevator systems, demonstrating that higher-tier designs could enable daily, propellant-free transfers to all planets, potentially revolutionizing interplanetary travel.
Contribution
It provides a detailed mathematical analysis of space elevator designs, identifying their capabilities and limitations for planetary transfers and proposing staged slingshot maneuvers for faster travel.
Findings
Tier 1 and 2 elevators enable transfer to outer planets with velocity gains.
Tier 3 elevators can provide daily transfers to all planets.
Counterweights can enhance velocity for interstellar travel.
Abstract
The construction of a space elevator would be an inspiring feat of planetary engineering of immense cost and risk. But would the benefit outweigh the costs and risks? What, precisely, is the purpose for building such a structure? For example, what if the space elevator could provide propellant-free (free release) orbital transfer to every planet in the solar system and beyond on a daily basis? In our view, this benefit might outweigh the costs and risks. But can a space elevator provide such a service? In this manuscript, we examine 3 tiers of space elevator launch system design and provide a detailed mathematical analysis of the orbital mechanics of spacecraft utilizing such designs. We find the limiting factor in all designs is the problem of transition to the ecliptic plane. For Tiers 1 and 2, we find that free release transfers to all the outer planets is possible, achieving…
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