[The Following is an excerpt from a letter to Allen Meece]
[Updated 4 September 2002]
I have a new suggestion for further reducing the VBP's
weight. We can change the shape of the balloons used from cylindrical to
the more common conical type which is proven its utility for low
operpressures.
This setup using conical balloons employs the same staggered
layout that we've been considering.
The maximum spacing between lift cells is only slightly less
than that for an array of vertical, cylindrical lift cells. The radii of
the cells must be greater for the same number of cells using conical
cells. However, the tapering of the bottom of the lift cells allows
them to be moored very close together without great compression or
reduction in volume. There is significantly less total
open space between the cells.
Most of the space between the balloons must be shielded by the
shroud so that the crew can work there. This means than open space between
the balloons represents additional cross sectional area for drag to act on
the platform.
A lift cell array of conical balloons has about half the
frontal surface area of one using the same number of cylindrical
balloons. This is a significant reduction in platform
drag.
A staggered arrangement of the lift cells is
useful because it props the lift cells up against being pushed around
by drag force. Keeping inflated balloons in contact lets the
friction of their contact act to keep them steady. And by properly
arranging the cut of the balloon fabric, we can allow orderly expansion of the
balloons during the ascent without their own expansion forcing them to rub
against one another. This staggered array is no different in this regard
than others we've examined.
As for motion of the balloons from side to side (as from
tacking or transverse waves in the array), a group of balloons moored at a
single point experiences less abrasion between the balloons than a group of
balloons in contact but moored at separate points.
The lift cells will tend to rotate about their mooring
point. Two lift cells moored at the same point will rotate in unison,
ideally with no relative motion. This is especially true if they begin
motion in contact over a large surface area, as greater contact area means
greater friction to resist motion relative to each other.
If moored at two separate points, the motion of balloon A need
not affect balloon B until A moves over far enough that it first contacts
B. This means that the angular momentum of two lift cells moored at the
same point is twice as much as a single lift cell. Thus, a single lift
cell rotates twice as fast in response to the same impulse.
If balloon A keeps moving, it will start B rotating as
well. Unfortunately, this pushing will cause A to rub against B is their
cross sections don't change. In B's reference frame, balloon A taps it at
point 1 and drags along its surface to point 2, imparting motion.
So, in addition to reducing forward surface area, an array of
conical lift cells is less prone to rupture due to abrasion by large
oscillations in the array because it reduces relative motion.
Another important advantage to this configuration is that it
can be expanded. If we suddenly find ourselves in need of 50% or so more
lift, we can raise additional balloons and hydrogen to the platform and deploy
them symmetrically along the sides.
The balloons would have to be deployed outside the shroud (not
shown here), but hopefully by that point the platform will be high enough to
bear the extra drag, and if the array is at full inflation they won't roll
around too much. The angle is a bit steep to expect no compression, but it
shouldn't be more than the array can handle.