Access to Fuel Tanks in the LTV Service Module
Although the service module shape carries through the shape of the
Spacehab modules, it is not really made up of Spacehab modules. What
you're really seeing is the outside of a thin membrane of multilayer
insulation (MLI). The MLI is a debris shield, supported on a flimsy wire frame.
It just looks robust. We make it sections and hinge each section to
form doors, which swing up to allow access to the fuel tanks. This is very
similar to the approach to the shielding used on the International Space
Station.
This image gives an idea of current thinking on the issue.
Once we can get oxygen and tanks from the moon, we can swap out those
tanks in lunar orbit. We'll launch hydrogen in fresh tanks from Earth.
Like the LTV scenario, we'll ferry the empties to lunar orbit and perhaps
even land them on the moon to be refilled.
A central truss runs down the length of the LTV Service Module.
The truss provides
attachment points for the tanks as well as support for fuel and thermal
control system plumbing, RCS rockets and their tanks, external avionics,
power and data wiring, and finally the engines with their gimbal
mechanisms, controllers, and pumps.
ASI W9601143r1.1.
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Updated Sat, Mar 7, 1998.