A Conceptual Study for the Autonomous Direct Forming of Lunar Regolith into Flexlock (Trademark) Geomats for Lunar Surface OperationsWe describe the conceptual method of an autonomously operable Direct Forming machine that would consume regolith or regolith slag to mold intimately, interlinked elements in a continuous process. The resulting product, one to three meter wide geomats, would be deployed over commonly traversed areas to isolate the astronauts and equipment from underlying dust. The porous geotextile would provide areas for dust settling, thereby mitigating dust impingement on astronaut suits or surface structures. Because of their self-supporting yet flexible structure, these geomats could be assembled into shields and buttresses to protect lunar habitants from radiation, forming a "flexoskeleton" from in situ materials.
Document ID
20110011491
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Robertson, Luke B. (NASA Kennedy Space Center Cocoa Beach, FL, United States)
Hintze, Paul (NASA Kennedy Space Center Cocoa Beach, FL, United States)
OConnor, Gregory W. (Amalgam Industries, Inc. Los Alamos, NM, United States)