What would be wrong with going ahead and finishing one of the original Space Shuttle options as a Heavy ?
Shuttle=C
More info & history
We have a pipeline now to supply external tanks, we have the present assets that are
used by the remainer of the shuttle fleet. We also have some of the assets that were to
have been used in launch operations to support both the Chalenger and the Columbia.
The Challenger was the one vehicle that was specially designed to support the polar orbit
that was needed for Military satelites, but never had the chance to be used as such.
We still have never launched a manned system into a polar orbit, nor have we retrieved
a vehicle from that orbital mechanism - it's quite complicated logistically.
First you loose the 'spin' that was added by earths gravitational field and rotation,
which causes you to have a significant reduction in mass to orbit capability.
But - there were graphite composite solid boosters that were developed only for use
in acheiving a polar orbit - not refurbishable like the steel casings that are routinely used,
They are considerably lighter than the steel ones, which gains back some of the lost
ability to dead lift weight to orbit. Remember - the only purpose of the solid boosters
is to lift the mass of the extermal tank until the velocity is established and the vshicle
has climbed high enough out of the gravity well to continue launch insertion.
Optimal burn for the solid boosters is 90 seconds.
Now with either a conventional Shuttle, or a Shuttle-C derivative, it would be wise
to allow the external tank to be inserted into a parking orbit for future use.
Where do we get the engines ? One original configuration called for the use of one
ot the OMS Pod type engines to be modified to burn Hydrogen and Oxygen and use
that to power the separated tank to parking position - robotically.
Where does the extra fuel come from ? The shuttle presently breaks away the lightning rod
which serves as part of the LOX Feed/GOX Vent mechanism, and this vented and pre-aimed
device pushes the forward end of the External Tank away from the Orbiter, and initiates the
tumble that causes it to break up and disinigrate upon re-entry.
There is in the neighbrhoof of 10,000 to 15,000 gallons of Oxygen left at this time, and
between 20,000 to 30,000 gallons of Hydrogen as well. Enough to reach the parking
orbit, and enough left over for use in generating electrical power and providing water
and a constituent of a breathable air mixture - just add some nitrogen and helium.
A combination of manned Shuttle Launches carrying connection module assemblies,
Shuttle-c's to dead lift equipment and supplies, brings another External Tank into the
arena each launch. We have had 113 Shuttle launches, and having lost Challenger
during the boost phase of the mission, we still could have had 112 External tanks to
pick from as candidates for mating and equiping as an orbital way-station.
The Moon may be a easier launch for mass than the earth one 6th the gravity, but
you've got to get a finished peice of equipment landed there, and assembled before you
can position it for any mining of mineral extraction operation.
Water ? Not there - no pressure of hydration to prevent evaperation and direct outgassing to space.
The trip to the Moon is a week each way - build a close orbit station first - large enough to do
something with, and develop a Moon Lab Base to transport and position on the lunar surface
after it has been assembles in an orbit that is only one day to get to and back from.
Then fly that finished facility to a landing where it can be expanded upon in following missions,
Then and only then will you have sufficient technology to persue the Mars lander concept.
We're talking a 3 year round trip - if nothing goes wrong.
"Open the Pod Bay door, Hal"