Main article: Space elevator

The construction of a space elevator would be a vast project, requiring advances in engineering, manufacture and physical technology.

Contents

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Overview

David Smitherman of NASA has published a paper that identifies “Five Key Technologies for Future Space Elevator Development”:

  1. Material for cable (e.g. carbon nanotube and nanotechnology) and tower
  2. Tether deployment and control
  3. Tall tower construction
  4. Electromagnetic propulsion (e.g. magnetic levitation)
  5. Space infrastructure and the development of space-based industry and economy

Two different ways to deploy a space elevator have been proposed.

Traditional way

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One early plan involved lifting the entire mass of the elevator into geostationary orbit, and simultaneously lowering one cable downwards towards the Earth’s surface while another cable is deployed upwards directly away from the Earth’s surface.

Tidal forces (gravity and centrifugal force) would naturally pull the cables directly towards and directly away from the Earth and keep the elevator balanced around geostationary orbit.

However, this approach requires lifting hundreds or even thousands of tons on conventional rockets, an expensive proposition.

Cable seeding design

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Please help improve this section by adding citations to reliable sources. Unverifiable material may be challenged and removed. (September 2008)

Bradley C. Edwards, former Director of Research for the Institute for Scientific Research (ISR), based in Fairmont, West Virginia proposed that, if nanotubes with sufficient strength could be made in bulk, a space elevator could be built in little more than a decade, rather than the far future. He proposed that a single hair-like 18-metric ton (20 short ton) ’seed’ cable be deployed in the traditional way, giving a very lightweight elevator with very little lifting capacity. Then, progressively heavier cables would be pulled up from the ground along it, repeatedly strengthening it until the elevator reaches the required mass and strength. This is much the same technique used to build suspension bridges.

The 18 tonnes needed for a seed cable may be resonably lightweight; the proposed average mass is about 200 grams per kilometer..

Loop elevator design

This is a less well developed design, but offers some other possibilities.

If the cable provides a useful tensile strength of about 62.5 GPa or above, then it turns out that a constant width cable can reach beyond geostationary orbit without breaking under its own weight. The far end can then be turned around and passed back down to the Earth forming a constant width loop, which would be kept spinning to avoid tangling. The two sides of the loop are naturally kept apart by coriolis forces due to the rotation of the Earth and the loop. By increasing the thickness of the cable from the ground a very quick (exponential) build-up of a new elevator may be performed (it helps that no active climbers are needed, and power is applied mechanically.) However, because the loop runs at constant speed, joining and leaving the loop may be somewhat challenging, and the carrying capacity of such a loop is lower than a conventional tapered design.

References

  1. ^ David V. Smitherman, Jr.. “Critical Technologies for the Development of Future Space Elevator Systems” (PDF). Retrieved on 2007-11-03. NASA Tech Report IAC-05-D4.2.04
  2. ^ Gassend, Blaise. “Exponential Tethers for Accelerated Space Elevator Deployment?” (PDF). Retrieved on 2006-03-05.

External links

  • Elevator:2010 Space elevator prize competitions
  • The Space Elevator Reference
  • Audacious & Outrageous: Space Elevators

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Categories: Exploratory engineering | Megastructures | Space colonization | Space technology | Vertical transportation devices | Space accessHidden categories: Articles needing additional references from September 2008 | All articles with unsourced statements | Articles with unsourced statements since September 2008 | Articles with unsourced statements since July 2008