[net.space] Lighter-than-air Launch

Nicholas.Spies@H.CS.CMU.EDU (01/18/86)

	 Given: We are at the bottom of the gravity well of the Earth
	 and also at the bottom of an ocean of air; the latter fact may
	 help to overcome the former. The 14 lbs/in^2 pressure of the
	 atmosphere [at sea level] is routinely used to generate lift;
	 but could this simple principle be used to develop
	 free-floating launch vehicles or large ground structures to
	 gain a decisive advantage for a space launch? (I acknowledge
	 that this is not an original idea as one of the first
	 proposals for spaceflight involved evacuated copper balls, if
	 I'm not mistaken, and also that some early rockets were launched
	 from ballons.)

	 It would seem that the ideal floatation medium would be
	 superheated hydrogen constrained by a tough, thin Mylar-like
	 film. A far safer but far more expensive next-best would be
	 superheated helium. Superheating in both cases would produce
	 higher pressures to counteract atmospheric pressure while
	 reducing the mass/weight of the lifting gas, increasing
	 lifting efficiancy. (Of course superheating would also
	 complicate the design of the envelope; perhaps heat
	 dissipation could be aided by introducing a small amount of
	 steam that could condense on the inner surface of the
	 envelope [or by taking off while raining!]).

	 At any rate, it would seem that a giant donut-shaped
	 lighter-than-air platform could, if large enough [how large?],
	 carry a fully-loaded shuttle to a fuel-saving altitude from
	 where it would be launched. Presumably "window-critical"
	 launches could be carried aloft, above most weather, from
	 where they could be launched on schedule. For the more
	 defense-minded, such platforms could presumably reside
	 indefinately in the upper atmosphere for a variety of
	 survaillance and defensive purposes.

	 Nearly-lighter-than-air structures might be a way of building
	 a ladder to space because traditional wisdom about the
	 strength of load-bearing members would be altered by the new
	 distribution of the load between compressive and floating
	 elements. Obviously such a structure would have to be designed
	 to take advantage of the tensile strength of materials, which
	 is typically many times greater than compressive strength.
	 Wind loading would increasingly be a more important factor,
	 which could be dealt with by distributing it to all other
	 elements of the structure and ultimately the ground. If we
	 were able to build a lasting tower 100 miles high (on a base
	 perhaps 50 miles across) able to support a shuttle-sized craft
	 would this realize much launch benefit? In the long term?

	 What are the critical problems with these proposals?

	 Nick Spies, Center for Art and Technology, CMU

space@ucbvax.UUCP (01/20/86)

We could get a good start just by climbing up existing mountains in
South America, Africa or Asia.  Imagine the top of Mount Everest
flattened off for a space port (:-)!