Sling-on-a-Ring: Structure for an elevator to LEO

TL;DR

This paper proposes a novel sling-on-a-ring space elevator concept that uses a high-tensile-strength orbital ring and long slings to efficiently transfer payloads to LEO, reducing mass in space compared to traditional designs.

Contribution

It introduces a new design for a space elevator using an orbital ring and long slings, with analysis on reducing structural mass for practical implementation.

Findings

Conceptual analysis shows potential for significant mass reduction.

Sling timing can detach payloads efficiently into space.

Use of advanced CCT fibers enhances structural strength.

Abstract

Various proposed space elevators may bypass the financial and environmental limits on rocket technology, but all have their own problems. A Low-Earth-Orbit, LEO, rotovator-based space-elevator version called 'sling-on-a-ring' may overcome them. This mass-lifting system uses the spatial stability of an orbital ring, accessorized for transfer and storage of momentum and electrical power. A high-tensile-strength equatorial circum-terra loop of colossal-carbon tube, CCT, fiber has solar-power and station-keeping units and rotating sling modules. Long sling assemblies, ~600 km, periodically descend into the atmosphere to ~13 km. At perigee, the sling rotational tip velocity almost cancels the orbital-ring velocity relative to Earth surface. Split-second timing detaches a ~10 ton payload from an ordinary aircraft and jerks it into space by sling momentum, with the proven specific strength of CCTs now under development. This system eliminates the immense mass in space of other space-elevator systems, but needs extremely long (~100km) compressive members. Conceptual analysis for mass reduction of these structures is the subject of this paper.