THINKING OUTSIDE THE MASS
FRACTION BOX
Part 1:
NASA’s Lunar Architecture Design Goals are Good,
but not quite what we need to Maximize our Lunar Presence Investment
By
Peter
Kokh
Moon Society Advisor and Videographer
Chip Prose had asked me to define the steps we need to take to realize
a human presence on the Moon to support a full buildout of an
Earth-Moon Economy. Actually, we have talked about most of the elements
and steps needed in various articles in MMM through the years.
Thinking within the “Mass
Fraction” Box guarantees failure
But it is a very worthwhile endeavor to
do the exercise afresh, and with deliberation. We’ll make a start with
this article, laying out basic concepts to “really maximize” the
payload delivered to the Moon. This means throwing out the window of
the slavishly worshiped law of “the mass fraction.”
According to
Wikipedia, “In aerospace
engineering, the mass fraction is a measure of a vehicle's performance,
determined as the portion of the vehicle's mass which does not reach
the destination. ... In rockets for a given target orbit, a rocket's
mass fraction is the portion of the rocket's pre-launch mass (fully
fueled) that does not reach orbit. ... typically around 0.8 to 0.9
[80-90% of the takeoff mass does not reach orbit]” The figure is even
more discouraging when we are considering the typical mass fraction
deliverable to the lunar surface.

The huge Saturn 5 in comparison to its tiny cargo, the lunar excursion
module
The goal, adopted by NASA, to design the
landing craft in such a way as to maximize delivered payload, is
excellent. According to the Connally Study:
- minimize ascent module mass
- minimize descent module mass
- maximize landed “payload” mass
- simplify interfaces
- move functions across interfaces when it makes sense
As we have seen in the Artemis Project's
use of a minimal open-cockpit "space motorcycle" crew ascent vehicle,
by use of a minimal ascent vehicle, NASA could land a much
more spacious crew cabin. But this is still a sample of thinking within
the Mass Fraction Box.
Thinking outside the
“Mass Fraction” Box, Part 1
When you think of it,
the payload “landed to remain on the Moon” in the Apollo missions
consisted only of the descent stage, and assorted equipment left
behind. Not much! NASA’s new “space-motorcycle”-inspired plan will
allow leaving the spacious crew cabin behind. That’s a big step, but
still within the “Mass Fraction Box.”
Our first article on “Thinking outside
the “Mass Fraction Box” was “Essays in ‘M’: Marshall MacLuhan: “Medium
is the Message” in MMM #6, June 1987. This is republished in MMM
Classic #1 - download from:
www.moonsociety.org/publications/mmm_classics/
In this article, we pointed out that the
most common flaw in thinking within the “mass fraction box” was to
assume without question that no part of the vehicle itself could be
reassigned as “payload.” We illustrate the possibilities by offering an
alternate configuration for the Space Shuttle Orbiter. I urge you to
download that volume cited above, if only to get this point across.
Here we are talking about delivery to the lunar
surface. In that context, our quest to cheat the “mass fraction” rules
drives us to make sure that everything that we have paid precious fuel
to land on the Moon, and which will not depart on the ascent vehicle,
is something that has more than temporary usefulness: that includes
every part of the landing platform mass:
- fuel tanks & descent engine & • vernier
rockets
- cargo hold & • unloading equipment
- leg struts & • foot pads, • etc.
There are several
approaches and types of solutions for this design challenge:
- The item can
be reused as is. For example, the bulk of the descent
platform, minus engines and fuel tanks, might be reused as a platform
for a telescope
- The item’s design
could be tweaked to enable it to serve some different
application, whether similar or quite different, for example, landing
struts could be assembled in line to use as an antenna mast, or
alternatively to serve as part of a space frame for a canopy shed
- Perhaps part
of the descent stage equipment could be designed as a
mobile chassis for the crew cabin, either to taxi the cabin to its
installation site, or to turn the cabin into a pressurized lunar
surface bus.
- The item could be forged
of a material that would be invaluable on the Moon, such
as lead, copper, brass, or stainless steel; some components, for
example shipping stuffs, could be made of reusable plastics, or
compressed biodegradables rich in nutrients scarce in lunar regolith
You get the idea. See “Stowaway
Imports,” in MMM # 65, May 1993, republished in MMM Classics #7,
downloadable from web address above.
We would be delighted to see the NASA Moon Lander
Office adopt these design goals also. This is not a new philosophy.
Poor people are known to use all parts of a slaughtered pig “except the
squeal!” NASA should and must adopt a “we are poor” posture, in the
sense that the agency will never get all the money it might want and
must learn to make do with what it gets. And to do that successfully,
means not to cut this and that, that’s a petulant knee jerk reaction,
but to exercise maximum resourcefulness. Use everything twice!
Note that our title reads:
“Thinking outside the “Mass Fraction” Box, Part 1” We hinted in our
reference to the article from MMM #6, that the launch vehicle itself,
and every stage of it, can be redesigned to add more to what lands on
the Moon and
contributes
to the buildup of the lunar outpost/settlement.
PART 2:
Improving on NASA’s Lunar Architecture Design Goals
In the first
installment last month, Part 1, we talked about making maximum use of
everything landed on the Moon. That way everything we land on the Moon
becomes payload delivered, not just the crew and cargo. Let’s carry the
argument further.
The Translunar Injection
Stage as a Deliverable
Any part of the Earth Orbit <> Lunar
Orbit ferry vehicle that delivers the landing craft to low lunar orbit
for its descent to the Moon’s surface, which is not needed
for the return to Earth orbit can be delivered the rest of the way to
the lunar surface at little extra cost. What things this may consist of
depends on the vehicle’s design. Expended fuel tanks (unless they are
refueled with lunar liquid oxygen) and farings are two obvious
suggestions. Of course, this implies that these items can be replaced
in LEO for the next trip out to the Moon.
In Apollo, the Saturn 3rd stage that
brought the LEM and Apollo Command Module was effectively tossed
overboard, left to crash on the Moon. (area in dotted box)
The SIVB: 58’ 7“ [17.85m] tall/long; 21’ 8” [6.6m] wide, such a volume
landed could provide ample storage, or, set on its side, a
spacious 2-floor habitat module. The adapter skirt covered the SIVB
engine and mated the SIVB to the Saturn 2nd stage.
This could be saved also.
Yes, to deliver this stage the rest of the way to
a soft landing on the Moon requires more fuel, but at least the oxygen
required could be brought up from the lunar surface. Delivered, this
adds large fuel tanks which could be put to welcome use in the
moonbase, plus an engine, cannibalizable wiring and other components.
Remember, we already paid the freight to get it almost all the way!
Those with shortsighted vision would not
want to bother, but if you are a prospective lunar pioneer, not to take
advantage of such a golden opportunity would be unforgivable, and as
lunar frontier history may someday judge, forever listed as an act of
unthinking treason against the future Lunar Republic.
We are not suggesting that the Lunar
Module ride to the surface atop this 3rd stage, though if we decided to
do that, the weight savings involved in not needing to equip the Lunar
module with its own separate descent stage engines and tanks, might go
a good ways toward paying for the extra fuel.
The equivalent of the Apollo Command Module needed
to return crew to Earth orbit or to Earth directly, could be dropped
off en route, breaking into lunar orbit, while the 3rd stage with lunar
module and minimalized ascent stage continued directly to the lunar
surface. It’s a different lunar architecture but the potential payoff
in “total payload delivered” is too great not to pursue. As we work out
the design and trade off particulars, a show-stopper problem may emerge,
but with the right attitude, we can bet that a doable workaround will
be found.
In the scenario above, even the farings
that protected the lunar lander on its trip up through Earth’s
atmosphere, could make the trip all the way. They would surely be
useful for one thing or another.
A Proper Guiding
“Philosophy” is essential
We must always keep in mind that maximum
total payload mass delivered is the Holy Grail. That implies, of
course, that we have predesigned every “hitchhiking” component to be
able to serve new uses and functions on the Moon, or have made that
component of a material that we cannot yet produce on the Moon, or may
never be able to produce, such as copper, brass, zinc, lead, and
reshapable thermoplastics, to name a few.
What about parts for which we can
foresee no reuse or reapplication potential? We can think of two
approaches right off the bat. Make them of materials needed on the
Moon. Store them up until someone does have use for them. At the very
least, they can be used in frontier sculptures, symbolizing the effort
it took to establish the frontier! Art is one very important way we
begin to accept our new surroundings as “home.”
Face it, we will not have bottomless
financial reserves, we will need to be spartan. Why not borrow the
operating principal used by the poor who need to use all of everything
that comes there way, in this example, a slaughtered pig -- “use
everything except the squeal.” To put it in more common
terms, we need to maximize and ramp up our “resourcefulness.”
This is not “Apollo II”
We need to remember that in the Apollo
program, the idea was not to establish a permanent base, but to conduct
a series of science “picnics” at scattered surface sites. In that
light, minimizing landed mass on the Moon was the proper design goal.
Now, as we pick one site and try to build it up to the point where it
becomes a truly functional complex serving a wide variety of operations
on a long term basis, everything changes. We will want to deliver as
much, not as little, as possible.
By including as second class payload, not just
crew, cargo, and initial cabin, but the entire landing craft and
perhaps the entire assembly that left Earth orbit bound for the Moon,
we demolish the Old “mass fraction limits” on deliverable payload. And
we demolish those limits at relatively little extra expense.
The payoff of adopting this design philosophy is that a given stage of
moonbase buildout can be reached in fewer trips from Earth, or
conversely, with the same number of trips from Earth, we can reach a
much larger, more complex and elaborate lunar outpost buildout.
This is important for an operation that
needs to maintain public and political support to continue. The more we
achieve with the lowest cost, the faster our presence on the Moon grows
first to a fully functional science and exploration outpost, then
towards one involving a growing number of civilians involved in
industrial operations aimed at tackling Earth’s energy and
environmental problems, the more surely it will survive changes in
political administrations, and congressional whims.
A parallel with the
Opening Act of the Universe
The only safe lunar outpost expansion philosophy
is an “inflationary” one, growing and evolving very fast, not very
slow. Until we reach a stage where our presence on the Moon can survive
periods of interrupted support from Earth, everything is tentative,
subject to a change in the winds that could mean a second retreat from
Luna.
Such a swift buildout approach will,
when all is counted up, be significantly less costly than a go slow,
pay as you go approach. Time is the most costly expense a of all. We
should know this from the Shuttle program. Initial cost per launch
figures where based on sixty launches per year, one every six days. Now
we are lucky to do four or five. But the expense of the standing army
of people needed for turnaround, as well as of management, never goes
down in proportion to mission rate.
Further, with each delay, inflationary
pressures come into place. To get our money’s worth we not only have to
reuse everything sent toward the Moon on the Moon, but we need to
buildout our lunar facilities and operations with all due speed.
The “Medium is the
Message”
We noted last month that extending
Marshal McLuhan’s dictum that the Medium is the Message to rocket
transportation and delivery architectures, the rocket itself can be
part of the payload, if properly designed, in all its parts, for useful
applications at the delivery site.
Meanwhile, the original second stage,
which delivers the moonbound stack to Earth orbit, should itself be
predesigned so that all its components can serve some useful function
in Earth orbit, building up the transportation hub with refueling,
assembly, and maintenance operations functions. We’ve already paid the
freight to deliver its fuel-expended dry mass to LEO. If we do not
leave it there and find someway to use it to ramp up orbital
operations, we are just tossing money away. Here too, we can treat the
Mass Fraction limits.
It begins to look as if the Mass
fraction rule was a product of neanderthal thinking. We got to where we
are by taking advantage of every opportunity, not by mindlessly
throwing opportunities away, because in our narrow horseblindered
professions we can’t see the possibilities!
PART 3 - Bootstrapping
through LEO and LLO with early lunar products

The Block & Tackle Pulley as an
Analogy of the Power of Leveraging
Concurrent Space Developments
to deliver much more to the Moon
“ in Earth orbit you are
halfway to anywhere” - Robert A. Heinlein
The “effective” cost of goods delivered to the lunar surface
depends on the amount, or lack of infrastructure along the way.
Archimedes invention of the pulley more
than 2200 years ago is one of the most important mechanical
contributions to early civilization. By realizing a predict-able
mechanical advantage, the “energy cost” of moving an object from one
plane, say Earth’s surface, to another, say the Moon’s surface is
significantly reduced. The block and Tackle pulley multiplies the
advantage.
What does this have to do with space
transpor-tation in general, and with the cost of delivery of goods from
Earth to the Moon in particular? We certainly are not talking
about setting up a physical block and tackle system in space! Rather we
want to apply the analogy above in a way that illuminates the best way
for us to proceed.
In short, transporting things to the Moon without
any intervening infrastructure, i.e. not cashing in any infrastructure
discounts or advantages, is going to remain very expensive. The “Moon
Direct” plan, if we can call it that, is the “horse blinder” choice.
“We are directed to put an outpost on the Moon, not to establish
infrastructure along the route.” What looks like dedication will
someday reveal itself to be an outright waste of resources and
opportunities. Future Lunans may even view it as criminal.
In parts of this article above, we have
noted that anything taken to orbit that might be useful in setting up
shop on the Moon, but left to fiery destruction as its orbit decays,
could be taken to the Moon at much less expense from LEO than from
Earth’s surface - if Heinlein is right, for about half the cost. And
that includes a lot of material, whether usable in its current form or
not. The deliberate “wasting” of the External Tank is but the most
obvious and long standing forfeit of opportunity. We fully understand
all the disadvantages and obstacles to reusing the ET. But they are
insignificant in comparison to what could have been gained by
commit-ting to the modest expense of parking them in a higher very long
duration orbit until the opportunity to use them in LEO or take them to
the Moon arose. As a Society, we have become addicted to favoring
short-term advantages over long-term goals, and such a habit, if we
don’t fight the addiction, could have us following the Romans into
oblivion. Again, I understand the excuses. But excuses are just what
they are.
The same holds true of anything else
delivered to LEO and GEO, which when no longer useful there, could be
delivered to the Moon at “half the cost.” LEO and GEO are pulleys in
any future fully developed lunar transportation system. So is the
Earth-Moon L1 Lagrange point and other lunar orbits. Anything delivered
that far that could be used, reused, restructured, or cannibalized on
the Moon will be far cheaper to deliver than an equivalent item all the
way from Earth.
The Lunar side of the
Block & Tackle
I remember Gordon Woodcock’s paper which
sought to prove that lunar oxygen used to refuel Moon-bound cargo
ships, could only reduce the cost of shipping to the Moon, but not make
it profitable. Duh!
What’s
wrong with reducing costs? Lunar oxygen, which is abundant
beyond exhaustion, can be shipped to L1 and to LEO with every returning
vehicle, to partially refuel each next Moon-bound craft. LOX is thus
another pulley in the system. As to LH2, which is not in large supply
on the Moon, we oppose shipping that off-Moon as fuel, or even for
using on the Moon as fuel, except for fuel cells in which hydrogen can
be recovered. Any shipment of hydrogen off the Moon limits the size to
which lunar settlements and biospheres can grow. In that perspective,
such shipment and usage becomes treasonable against the Lunan Frontier.
Lunar Exports
Many people point out that the Moon has
nothing of value “on Earth” except perhaps Helium-3, and maybe platinum
(I am very dubious of this latter idea.) What these people are failing
to understand is that the logical export partner of the Moon, is not
Earth, but LEO. Anything that can be made on the Moon to fit service
needs in LEO can be shipped to LEO at a 20:1 fuel cost advantage over
shipment of equivalent goods up from Earth’s surface. Of course, that
statement does not factor in the need to amortize the costs of
developing lunar industries needed to export such items. That does not
change the argument, however.
Items made of concrete, cast basalt, glass, alloys
of steel, aluminum, magnesium, and titanium are candidates. Yes, there
will be some specialty materials that lunar industries won’t soon be
able to match. But in designing LEO installations - space stations,
laboratories, factories, tourist facilities, whatever, if the design
team tweaks the design to use lunar products, the cost savings will be
considerable. Even dehydrated food, over 50% lunar oxygen by weight,
can be shipped more cheaply to LEO than from Earth! The point is, that
all these export products will help defray the cost of shipping things
in LEO the rest of the way to the Moon. Another Pulley!
Not to forget GEO
GEO -- Geostationary Earth Orbit -- is
long overdue for wholesale restructuring of the way the limited and
invaluable slots along this orbit are assigned and utilized. With large
platforms supplying power and station keeping, serviced by robotic
tugs, many communications and other GEO satellites can share the same
orbital slot, taken to the platform by the tug, and “plugged in.” GEO
is almost saturated in our present “hunter-gatherer” level of alotting
space. How will products from the Moon help?
We already understand that lunar
materials can bring down the cost of solar power satellites and relays
in GEO by substantial proportions. [See last month’s MMM proposal for a
World Wide Orbital Grid.] These same materials can help build new and
larger platforms for communications and other uses. And the tugs needed
will be of use as well in LEO in maximizing reuse and salvage of items
in orbit, including gathering them for transshipment to the Moon. GEO
platforms, power systems and tugs -- another Pulley”
“Mechanical” Cost
Advantages
Any estimate of what it will cost to
open the Lunar Frontier, that neglects the opportunities to ship to the
Moon anything shipped to LEO, GEO, or other points in between and no
longer needed at those points, or which neglects to credit exports from
the Moon to LEO, GEO, or other points between will necesarily
be fantastically outlandish.
At the same time, we are not saying that opening
the Lunar Frontier will quite pay for itself in the near future. That
said, we are confident it will do so much more quickly than most
authorities now estimate. Those less optimistic predictions are a
natural, given the human tendency to be too optimistic in predicting
the near-term future and far too pessimistic in predicting the
long-term future.
I was asked recently to outline “The Ten
Steps Needed to Create an Earth-Moon Economy.” I dislike pre-set
outlines. Whether it is five steps or fifty is uncertain. But this set
of articles on “Thinking outside the Mass-Fraction Box” are my first
installment towards an answer to that request. In other words, we are
not going to succeed in setting up an Earth-Moon economy
without paying attention to “the pulley points” along the way.
LEO & GEO can
only be fully developed
using the significant cost advantage
of Lunar materials and exports.
The Moon cannot be fully
developed without
access to materials and items shipped to LEO
which when they are of no further use there,
are then transshipped to the Moon.
The first Step: a
refueling station in LEO
At the 2007 International Space
Development Conference in Dallas over the Memorial Day Weekend, Dallas
Bienhoff of Boeing gave a convincing presentation that simply by
refueling Moon-bound craft in LEO, we could deliver 60% more goods for
the money. Please view the three video segments produced by the Moon
Society in which Bienhoff explains his thesis.
http://www.youtube.com/watch?v=_WxvIk463P0&feature=related
http://www.youtube.com/watch?v=m6H9G0eh1vc&feature=player_embedded
http://www.youtube.com/watch?v=N-cFfPUjKpU&feature=related
Bienhoff is correct in saying that NASA
has an obligation to identify the least expensive way back to the Moon.
However, that constraint imposed by Congress, is shortsighted, in words
we all know, “pennywise and pound foolish.” The current
Spartan approach can only be defended if setting up a lunar outpost is
a goal in its own, without considering further use of that outpost, or
further lunar developments.
Many years ago, I wrote in an In Focus
editorial which I can’t locate at the moment, that the space enthusiast
community has all too often attempted to sell the ladder of our dream
one rung at a time. When we do that, the rung in question gets designed
as a be-all and end-all in itself, not as a rung leading to the next
rung, not as part of the ladder. Thus we have only ourselves to blame
for the Space Station becoming a black hole for funding, leading
nowhere. In the selling of the Station, it became not a depot to outer
space as conceived of by Wernher von Braun, but a downward looking
Earth-research laboratory, the pride of “yo-yo space.” We were afraid
that if we talked about our real dream, no one would listen. The result
of this space enthusiast consensus strategy of the early eighties is
20-some years since of going nowhere.
If we promote the NASA permanent, but
not permanently occupied, science outpost as a goal in itself, that’s
what it will become. Because we can’t allow ourselves as a nation to
look further down the road, we will continue to make stupid
shortsighted decisions which will only bring further delays to opening
the Moon.
Anything that is worth doing is worth doing right.
We have to rethink the NASA moonbase as a rung in a ladder, that means
flushing LAT-2 down the LATrine. It’s a quite brilliant design intended
to lead to nowhere.
Ten Steps to an Earth-Moon Economy? It
includes building up a block-&-tackle-reminiscent set of cost
savings enhancers in LEO, GEO, L1, and on the Moon itself. And it
includes dumping LAT-2 constraints. NASA has rightfully canceled
further biological life support system research as not of use for its
current concept of the lunar outpost. Can there be any more eloquent
clue that the agency is off track, way off on a tangent?
NASA itself admits the potential for
using lunar resources, but has chosen for this Congressional
assignment to constrict its vision to what is pertinent for the
mission so defined. In its dedication, NASA has unwittingly chosen to
become part of the problem. Yet the agency has enormous expertise and
problem solving resources. It needs a change in direction that
unleashes those talents. Perhaps the next administration will see to
that. In the Apollo program, NASA was at its prime. Under present
leadership, the agency is playing a caricature role, expertly. But this
is the price we pay for a space program that continues to be a
political football.
We, those of us in the bleachers, disparaged by
NASA and the government alike, have to be vigilant for ways to make an
end run around what is happening. The LEO and GEO and even Lunar export
options we have mentioned will be the work of private enterprise.
That’s our point of entry. Optimism has to be earned.
<MMM>