A strong attractive feature of form stiffened shells is their ability to be
compactly roll stowed. The resulting tubular or column like storage factor
should lend itself to efficient integration into payload volumes and is
also an inherently strong structural element enabling the aperture to
better survive launch loads while minimizing the amount of surface area
exposed to acoustic loadings. Perhaps most important, at least for
membrane optical applications, is the fact that no folding operations are
needed to stow such an aperture. This eliminates the potential for creases
that could permanently scar the surface finish and/or require larger
deployment forces to straighten the surface and pull out the creases.
The exact limit on roll stowage inner diameter (and hence overall stowage
diameter) depends on material and coating limits.
The roll stow approach could be used to package and launch circular
apertures or surfaces of upwards of 18 to 20 meter diameter (assuming the
Shuttle or Delta 4 Heavy Dual Manifest, for example) could be stowed within
existing launch vehicle fairings. If elliptical or oval outer perimeter
shapes were tolerable, achievable deployed size could likely be doubled
along one axis (i.e. apertures that are 20 x 40 in rough shape).
Alternative stowage methods that further increase achievable surface area
and/or diameter have also been developed and validated with proof of
concept experimental results.