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A small scale lunar launcher for early lunar material utilizationA system for the launching of lunar derived oxygen or raw materials into low lunar orbit or to L2 for transfer to low earth orbit is presented. The system described is a greatly simplified version of the conventional and sophisticated approach suggested by O'Neill using mass drivers with recirculating buckets. An electromagnetic accelerator is located on the lunar surface which launches 125 kg 'smart' containers of liquid oxygen or raw materials into a transfer orbit. Upon reaching apolune a kick motor is fired to circularize the orbit at 100 km altitude or L2. These containers are collected and their payloads transferred to a tanker OTV. The empty containers then have their kick motors refurbished and then are returned to the launcher site on the lunar surface for reuse. Initial launch capability is designed for about 500T of liquid oxygen delivered to low earth orbit per year with upgrading to higher levels, delivery of lunar soil for shielding, or raw materials for processing given the demand.
Document ID
19820052082
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Snow, W. R.
(Princeton Univ. NJ, United States)
Kubby, J. A.
(Princeton Univ. NJ, United States)
Dunbar, R. S.
(Princeton University Princeton, NJ, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1981
Subject Category
Astronautics (General)
Meeting Information
Meeting: Space manufacturing 4
Location: Princeton, NJ
Start Date: May 18, 1981
End Date: May 21, 1981
Accession Number
82A35617
Funding Number(s)
CONTRACT_GRANT: NSG-3176
Distribution Limits
Public
Copyright
Other

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