Poster's note: Isn't this just a reformatted version of the Aurora
flight report?  If so, it ignores gas guns (which are half the price
in $/kg of solid-propellant guns) and contradicts SPICE balloon cost
estimates.  It works up aircraft way more than other tech, leading to
unsurprisingly lower cost estimates of these technologies.  Coming up
with low prices for worked up tech seems a common thread in papers.
This could be clarified by authors generally, I feel.

http://iopscience.iop.org/1748-9326/7/3/034019

We perform engineering cost analyses of systems capable of delivering
1–5 million metric tonnes (Mt) of albedo modification material to
altitudes of 18–30 km. The goal is to compare a range of delivery
systems evaluated on a consistent cost basis. Cost estimates are
developed with statistical cost estimating relationships based on
historical costs of aerospace development programs and operations
concepts using labor rates appropriate to the operations. We evaluate
existing aircraft cost of acquisition and operations, perform in-depth
new aircraft and airship design studies and cost analyses, and survey
rockets, guns, and suspended gas and slurry pipes, comparing their
costs to those of aircraft and airships. Annual costs for delivery
systems based on new aircraft designs are estimated to be $1–3B to
deliver 1 Mt to 20–30 km or $2–8B to deliver 5 Mt to the same altitude
range. Costs for hybrid airships may be competitive, but their large
surface area complicates operations in high altitude wind shear, and
development costs are more uncertain than those for airplanes. Pipes
suspended by floating platforms provide low recurring costs to pump a
liquid or gas to altitudes as high as  ~ 20 km, but the research,
development, testing and evaluation costs of these systems are high
and carry a large uncertainty; the pipe system's high operating
pressures and tensile strength requirements bring the feasibility of
this system into question. The costs for rockets and guns are
significantly higher than those for other systems. We conclude that
(a) the basic technological capability to deliver material to the
stratosphere at million tonne per year rates exists today, (b) based
on prior literature, a few million tonnes per year would be sufficient
to alter radiative forcing by an amount roughly equivalent to the
growth of anticipated greenhouse gas forcing over the next half
century, and that (c) several different methods could possibly deliver
this quantity for less than $8B per year. We do not address here the
science of aerosols in the stratosphere, nor issues of risk,
effectiveness or governance that will add to the costs of solar
geoengineering.

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