1)    At first; as many components as possible (particularly the cryo
valves) should be off the shelf.

2)     I am guessing that the LOX should either be atomized or at least put
into a very fine spray and possibly not injected solely at the top of the
motor.

3)    I think the plumbing should be rigid due to the extreme temperature
differences the system will see.

4)    A well built spin caster would give us quick repeatability with the
fuel grains and could possibly be built in such a way as to be portable.
i.e. mounted to a trailer for trips to the desert or promo opportunities.

5)    I am curious if the strange post-burn parrafin geometry is due to too
much transient heat during the burn.  If so; could we run cryo plumbing
around the motor casing and keep the parrafin cold and solid everywhere but
the burn surface?  If so; would this change the burn characteristics of the
parrafin?  (i.e. ignition temp, burn rate, etc.)

6)    Probably a question for Andrew, but can we set the rocket up so that
if the initial nav system detects a noticable change in direction (+ or -
som many degrees from the vertical) the LOX feed shuts off and the chutes
are deployed?  I think that a system of this size and complexity might have
some balance issues.

7)    Intellectual property rights NEED to be discussed.  I know that some
of us would love to see this develop into some sort of business venture in
the future.