Mars: A Future Home for Humanity chapter two
MARS DIRECT
(c) Robert Zubrin & Chris McKay
Here's how the Mars Direct plan works. At an early launch
opportunity - 1999, for example - a single heavy lift
booster with a capacity equal to that of the Saturn 5 used
during the Apollo program is launched off Cape Canaveral. It
uses an upper stage to throw a 40 tonne automated payload
onto a trajectory to Mars. Arriving at Mars eight months
later, the payload vehicle aerobrakes into orbit around Mars,
and then lands with the help of a parachute. This payload is
the Earth Return Vehicle (ERV). It flies out to Mars with its
two methane/oxygen propulsion stages unfueled. In addition,
it carries six tonnes of liquid hydrogen cargo, a 100
kilowatt nuclear-reactor mounted in the back of a
methane/oxygen-driven light truck, a small set of compressors
along with an automated chemical processing unit, and a few
small scientific rovers.
On landing the truck is telerobotically driven a few hundred
meters away from the site, and the reactor is deployed to
provide power to the compressors and chemical processing
unit. The hydrogen brought from Earth can be quickly reacted
with the Martian atmosphere, which is 95 percent carbon
dioxide (CO2) gas, to produce methane and water. This
eliminates the need for long term storage of cryogenic
hydrogen on the planet's surface. The methane so produced is
liquefied and stored, while the water is electrolysed to
produce oxygen, which is stored, and hydrogen, which is
recycled through the methanator. Ultimately these two
reactions (methanation and water electrolysis) produce 24
tonnes of methane and 48 tonnes of oxygen.
Since this is not enough oxygen to burn the methane at its
optimal mixture ratio, an additional 36 tonnes of oxygen is
produced via direct disassociation of Martian carbon dioxide.
The entire process takes ten months, at the conclusion of
which a total of 108 tonnes of methane/oxygen bipropellant
will have been generated. This represents a leverage of 18
to 1 of Martian propellant produced compared to the hydrogen
brought from Earth needed to create it. The ERV requires 96
tonnes of the bipropellant for fueling, leaving 12 tonnes
available to support the use of high powered chemically
fueled, long range ground vehicles. Large additional
stockpiles of oxygen can also be produced, both for breathing
and for turning into water by combination with hydrogen
brought from Earth. Since water is 89% oxygen (by weight),
and since the larger part of most foodstuffs is water, this
greatly reduces the amount of life support consumables that
need to be hauled from Earth.
In 2001, following the successful completion of the vital
propellant production on Mars, two more boosters lift off
the Cape and throw their 40 tonne payloads towards Mars. One
of the payloads is a fuel-factory/ERV, just like the one
launched in 1999. The other is a habitation module
containing a crew of four, a mixture of whole food and
dehydrated provisions sufficient for three years and a
pressurized methane/oxygen ground rover. On the way out to
Mars, artificial gravity can be provided to the crew by
extending a tether from the habitat to the burnt-out
booster's upper stage, and spinning the assembly.
Upon arrival, the crew's craft drops the tether, areobrakes
and lands at the 1999 landing site where a fully fueled ERV
and fully characterized and beaconed landing site await it.
With the help of such navigation aids, the crew should be
able to land right on the spot. But, even if the landing is
off course by tens or even hundreds of kilometers, the crew
can still achieve the surface rendezvous by driving over in
their rover. If they are off by thousands of kilometers, the
second ERV provides a backup. However assuming the landing
and rendezvous at site number one is successful, the second
ERV will land several hundred kilometers away to start making
propellant for a 2003 mission, which in turn, will fly out
with the additional ERV to open up Mars landing site number
three.
Thus, every other year two heavy lift boosters are launched,
one to land a crew, and the other to prepare a site for the
next mission. WITH AN AVERAGE LAUNCH RATE OF JUST ONE BOOSTER
PER YEAR, WE CAN PURSUE A CONTINUING PROGRAM OF MARS
EXPLORATION. This is only about 10 percent of the U.S. launch
capability, and is clearly affordable. In effect, the dog
sled approach removes this dogsled approach removes the human
Mars mission from the realm of mega-fantasy and reduces it to
practice as a task of comparable difficulty to that faced in
launching Apollo missions to the Moon.
The crew will stay on the surface for one-and-one-half years.
Unlike conventional Mars mission plans based upon orbiting
motherships with small landing parties, no-one has been left
in orbit, vulnerable to the hazards of cosmic rays and
zero-gravity living. Instead, the entire crew will have
available to them the natural gravity and protection against
cosmic and solar radiation afforded by the Martian
environment, so there is no strong motive for a quick
departure. The mobility afforded by the ground vehicles will
allow the crew to accomplish a great deal of surface
exploration. With a 12 tonne surface fuel stockpile, they
have the capability for more than 25,500 kilometers traverse
before they leave. At the conclusion of their stay, the crew
return to Earth in a direct flight from the Martian surface
in the ERV. As the series of missions progresses, a string of
small bases is left behind on the Martian surface, opening up
broad stretches of territory for human exploration.
Such is the basic Mars Direct plan. By taking advantage of
the most obvious local resource available on Mars - its
atmosphere - the plan allows us to accomplish a human Mars
mission with what amounts to a Lunar class transportation
system. By eliminating any requirement to introduce a new
order of technology and complexity of operations beyond those
needed for Lunar transportation to accomplish piloted Mars
missions, the plan can reduce the cost of the Space
Exploration Initiative by an order of magnitude and advance
the schedule for the human exploration of Mars by a
generation.
Purists may object that Mars Direct doesn't go completely
native. After all, the plan brings the reactor's energy, the
ERV's hydrogen and part of the crew's food from Earth. On
the other hand, while Amundsen may have lived of caribou and
travelled by dogsled, he did his hunting with modern rifles
and brought skies (a uniquely Norwegian innovation) along
too. Its necessary to be practical. Utilization of Martian
resources beyond the freely available carbon dioxide
"caribou" will come in the course of larger scale bases and
settlements.
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