Crossman_2006abstr
Copyright © 2006 by Frank Crossman. Published by
the Mars Society with permission
THE
WEAKEST LINK IN THE SPACE ELEVATOR VISION -
CARBON
NANOTUBES
Frank W. Crossman
ABSTRACT
The
space elevator, hypersonic tether, and related concepts offer the promise of
reducing the cost of reaching earth orbit by a factor of 10. There has been
growing interest in the development of concepts for a space elevator ribbon
made from carbon nanotubes (CNTs) that supports robotic climbers capable of
traveling a few hundred km/hr on a several days
journey to earth geosynchronous orbit (GEO) and beyond. Although the proponents
readily agree that the only material from which an
elevator can be made is CNT material with a theoretical strength of ~1/10 its
measured stiffness of approximately 1 TPa, nearly
everyone has ignored the critical fact that theoretical strength is based on
the assumption of perfect crystalline structure not only at the nanometer
scale, but also extending to the macroscopic (meter scale) and even to the
"GEOscopic" (36,000 km scale).
The
observed facts are that all materials are found to contain defects at
several scales that reduce the effective macroscopic strength of materials to ~
1/100 of the crystalline stiffness. The proponents of space elevator would like
to believe that CNTs are an exception to this rule. But since the year 2000,
experiments on CNTs have shown that this material is not an exception to the
rule - carbon nanotubes do contain defects. Furthermore, the shear strength and
shear stiffness of parallel arrays of CNTs are two orders of magnitude less
than tensile strength and stiffness along the tube axis. This paper will
review the physics of CNT crystalline anisotropy and the fracture mechanics of
several types of defects found in CNTs and in macroscopic aggregates (ropes,
ribbons) made from CNTs. The implications of these defects on the projected
strength of macroscopic CNT structures and their use in space elevators and
tethers for Earth and Mars will be discussed.