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Technical Paper

Proposed Androgynous Docking Airlock/Utility Module

2009-07-12
2009-01-2585
This allows the module to impose the least stowage penalty within the launch shroud and also the least mass, thus, it can be launched by a relatively small booster utilizing the smallest payload fairing dimensions. On the forward and aft ends of the inflatable, cylindrical ADAM module are rigid structural hemispheres with a docking adaptor on the side interfacing to the Orion Vehicle.
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