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Space Transportation - mmmt_transportation.pdf - Moon Society

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The frog/toad/coach arriving on site could (1) be designed to hard-dock, in which case it must (a) be able to<br />

level, orient, and align itself properly for the task, and (b) be able to either lock or deactivate its suspension, perhaps<br />

with retractable legs. (If the suspension were allowed to continue floating, the hard-dock seal would be under<br />

continual stress with personnel moving back and forth.) Alternately, the vehicle could (2) be designed to link-up with<br />

the shelter via a some-what flexible and alignment-forgiving, short pressurized vestibular passageway (a) extending<br />

from itself to the shelter, or more logically (b) tele-extended from the shelter to itself by a prompt from within the<br />

vehicle. There would seem to be engineering, weight, and safety tradeoffs between these hard- and soft-dock options<br />

and we do not suggest which would be the more practical in the short run..<br />

[One criticism of our frog concept brought to my attention at the conference was that, as illustrated, it involved a<br />

pair of widely separated engines, one to either side of the centrally suspended mobile crew pod, introducing<br />

potential instability if either engine had to be shut down for any reason. Our response is simply that there is so<br />

much to be gained by using frog-like vehicles - however they be configured - that it is very much worth the trouble<br />

to find or develop engineering work-arounds of this problem feature (e.g. a single top center engine with the<br />

exhaust split between pod-flanking exhaust bells). By hook or by crook, there has to be a way! - PK]<br />

Outfitting constraints<br />

To play its part, the coupling vehicle be out-fitted in a way that the capabilities it offers are complementary to<br />

those offered by the hostel shelter. It would seem that the repertoire offered would vary according to the customary<br />

length of trip for which the vehicle was designed. The possibilities suggest two general classes, the ‘commuter and the<br />

traveler.<br />

(1). Commuter class vehicles would include shuttle craft plying between the lunar surface and either an<br />

orbiting depot or a more substantial orbiting mother craft such as an Earth to <strong>Moon</strong> (or LEO to LLO) ferry. Also fitting<br />

the description would be suborbital hopper linking mutually remote lunar sites. In either case the commuting craft is<br />

occupied for only a few hours at time. Thus it may not contain berth space, galley (though food stores are likely to be<br />

a major part of the cargo), or head, though some emergency-use only arrangements would be a prudent option<br />

should the craft go astray or be forced to land far from its destination.<br />

Even here, we have a vehicle which could bring something to a hostel partnership. For both shuttle or hopper<br />

will have communications, navigation, and computing equipment which do not need to be duplicated in the hostel.<br />

And either will likely have an emergency first aid compartment complete enough to serve the crew in its hostel stay, as<br />

well as other emergency survival provisions. Finally, its air recycling equipment (a water recycling capacity is less<br />

likely) and ventilation fans, might easily be oversized without too much weight penalty, so as to also serve the hostel<br />

space well enough in a close-coupled configuration.<br />

(2). Traveler class vehicles would include such landing craft comprised of a shuttle module delivering a<br />

“through-cabin” crew-pod transferred from an Earth-<strong>Moon</strong> (LEO-LLO) ferry. As on the coast to coast Pullman sleeper<br />

cars passed on from one railroad to the next in an era now long gone, the crew coming to staff the hostel would ride<br />

the same “through-cabin” all the way from LEO, or even all the way from the Earth’s surface.<br />

Also in the cruiser category is the “overland” coach (from an established settlement or full base) designed for<br />

trips cross-lunar excursions of a day or more in duration. In either scenario, the visiting craft will contain serviceable if<br />

cramped “hot-rack” berth-space that can serve in the hostel-hookup as emergency infirmary beds if isolation or<br />

quarantine is called for. And certainly the craft will have at least a minimally equipped galley and head (possibly with<br />

shower) as well as a compact entertainment center with some recreational extras. Such more fully equipped vehicles<br />

would serve especially well as hostel complements, leaving the hostel to provide what it can offer most economically<br />

and efficiently: hard shelter from the cosmic elements, and plenty of elbowroom to serve the less expensive low-tech<br />

but space-appreciative aspects of daily life -- private bedrooms and communal areas for dining, gaming, exercising,<br />

etc. ><br />

MMM #51 - December 1991<br />

HYBRID RIGID-INFLATABLE STRUCTURES IN SPACE<br />

By Peter Kokh<br />

In last month’s MMM, we explored some possible architectures that could be useful in realizing the froghostel<br />

concept for lower threshold, timelier, less expensive yet more extensive lunar occupancy. One of the promising<br />

avenues looked at was the idea of rigid-inflatable hybrids in which the rigid component was packed with systems<br />

modules and the inflatable component providing habitat and activity volume - all in one ready-to-deploy package.<br />

There is no reason why this concept wouldn’t work for space structures just as well as for lunar surface<br />

outposts. And indeed there have been some precursor ideas. At the 1990 <strong>Space</strong> Development Conference in Anaheim,<br />

California, J.R. Thompson, then deputy NASA Administrator, shared with us some of his surprisingly unfettered<br />

thoughts about real near-term possibilities. Thompson felt there was no reason why the Shuttle orbiter, refueled in<br />

11

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