THE ARTEMIS PROJECT
PRIVATE ENTERPRISE ON THE MOON
TransLunar Transportation System
Section 4.2.1.
Home Tour Join! Contents Team News Catalog Search Comm

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.

LTV Service Module
 showing access doors for replace fuel tanks

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.

TransLunar Transportation System

Home Tour Join! Contents Team News Catalog Search Comm
ASI W9601143r1.1. Copyright © 2007 Artemis Society International, for the contributors. All rights reserved.
This web site contains many trade names and copyrighted articles and images. Refer to the copyright page for terms of use.
Author: Gregory Bennett. Maintained by ASI Web Team <asi-web@asi.org>.
Submit update to this page. Maintained with WebSite Director. Updated Sat, Mar 7, 1998.