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Please use this identifier to cite or link to this item: http://hdl.handle.net/1853/8047

Title: A Solar-Powered Near Earth Object Resource Extractor
Authors: Rangedera, Thilini
Vanmali, Ravi
Shah, Nilesh
Zaidi, Waqar
Komerath, Narayanan Menon
Georgia Institute of Technology. Space Systems Design Lab
Georgia Institute of Technology. School of Aerospace Engineering
Subjects : Near Earth Objects
NEO
Solar-powered robotic craft
Reconfigurable solar sail and collector
Solar-powered propulsion and power sources
NEO material excavation
Neodymium fiber laser beam
NEO resource processing
Issue Date: 10-Nov-2005
Publisher: Georgia Institute of Technology
Series/Report no.: SSEC05. Session F;GT-SSEC.F.3
Abstract: This paper is an offshoot of a project to study means of forming massive radiationshielded structures using Near Earth Object (NEO) materials. The topic is the conceptual design of a solar-powered robotic craft to land on, attach to, and extract materials from, a typical NEO. A solar-powered trajectory to a candidate NEO is used to estimate requirements. A reconfigurable solar sail / collector is the primary propulsion and power source for the craft. Following a journey of nearly 5 years, the craft will use a unique pulsed plasmajet torque-hammer concept to attach to the NEO. The basic cutting tool element is a solar-powered Neodymium fiber laser beam sheathed in a plasma jet, expanded through a truncated aerospike nozzle. Two telescoping, rotating arms carrying a total of 60 such nozzles at the ends of "fingers" enable the craft to dig and "float" out NEO material at a rate adequate to build a 50m diameter, 50m-long, 2m thick, walled cylinder within 19 days. The system is also amenable to applications requiring excavation of a large mass of near-surface material for resource processing. The present design appears to close with a total payload to LEO of 37,500 kg, with a total mass of 30,000 kg including the sail/collector at earth escape. The primary consumables on the system are the plasma gas for cutting and maneuvering, and electrodes of the plasma cutters.
Description: This conference features the work of authors from: Georgia Tech’s Space Systems Design Lab, Aerospace Systems Design Lab, School of Aerospace Engineering, Georgia Tech Research Institute; NASA’s Jet Propulsion Laboratory, Marshall Space Flight Center, Goddard Space Flight Center, Langley Research Center; and other aerospace industry and academic institutions
Type: Presentation
URI: http://hdl.handle.net/1853/8047
Appears in Collections:SSEC05. Session F: University Session II
Space Systems Engineering Conference (1st - Atlanta - 2005)

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