I've entered my designs for a solar vacuum airship in the Design the Future Contest. A more detailed writeup will follow, but here is the entry abstract:
Many locations with poorly developed infrastructure do not have the
capacity to receive airplanes and rely on ground transport from better
equipped ports. Conventional airships could theoretically put down at
any location, but due to expense of helium lifting gas are rarely used.
They are also difficult and dangerous to handle during landing and
take-off. To overcome these difficulties use of a vacuum airship is
Instead of a lighter than air gas, rigid vacuum
vessels are used; once air is removed from these vessels, net weight of
the vehicle is reduced. Rather than a complex air bladder system, five
separate vacuum “tanks” are proposed. This system allows pilots to
control vehicle density and weight distribution by adjusting pressure,
and therefore weight, in each tank. As air is removed the vehicle rises
and it drops when air is vented into the tanks, a system which allows
Once at its target altitude the vacuum pumps can be shut
off and the vehicle is able to cruise indefinitely. This is achieved
by covering the external surface with shaped solar cells. This improves
the airship's drag profile while generating power for onboard control
systems and electric motors used for propulsion.
Excess power is
stored by converting water into hydrogen through electrolysis.
Hydrogen is then saved until solar power is unavailable, and used in
fuel cells. This system allows a vehicle to be easily scaled in terms
of power and duration. Additional fuel cells provide additional power
much more efficiently than batteries and extra hydrogen storage can be
added to improve range when sunlight is unavailable. Very little water
is lost during this process and losses can be supplemented by use of
outer skin condensate collection.
To improve the drag profile
the carriage seen on conventional airships is removed. Instead a hollow
keel is suggested, connecting the various components. In addition to
providing the backbone, this keel also acts as the crew area and cargo
The reference vehicle proposed here is a cargo airship
capable of carrying 50 metric tons at a cruise altitude of 10
kilometers. This altitude is chosen as it is above most heavy cloud
cover and weather effects, allowing maximum use of the solar cells. It
is 360 meters long and 72 meters wide, a ratio chosen for its optimal
drag characteristics. Each of five 36 meter radius vacuum tanks has a
total volume of 195,000 cubic meters. It has 65,000 square meters of
solar cells powering three 240 kilonewton engines. Total interior cabin
volume comes to 4,000 cubic meters. Maximum velocity is 120 kph,
although recommended cruise velocity is 85 kph.
reference airship suggested here is intended for carrying people and
cargo to remote, underdeveloped areas; it is a versatile design that can
be used for a number of other applications. It could be readily
modified into a cruise ship or used as a research vessel. Potential
military applications include use as a naval radar platform and as a
long-range surveillance vehicle.