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Construction of large space structuresThe paper examines a construction capability to build large structures in space, its use in conjunction with the Shuttle Orbiter and a large Space Construction Base, and its relationship to system performance and cost. The geodetic beam design using a tetrahedral truss structure and reinforced plastics and its structural analysis, tests of demonstration cylinders, and preliminary machine design are discussed. The geodetic structure is shown to have high buckling stability, low thermal distortion, high stiffness, and its simple shape permits high-production-rate automatic fabrication. The geodetic beam fabrication machine which will automatically fabricate cylindrical beams in space from earth-prefabricated rods, and on-orbit beam and platform fabrication are described. Preliminary results of system performance and cost studies indicate that on-orbit fabrication using a small geodetic beam machine can be economically superior to the deployable and erectable modes of construction for many near term applications.
Document ID
19790069285
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Garibotti, J. F.
(McDonnell-Douglas Astronautics Co. Huntington Beach, CA, United States)
Cwiertny, A. J., Jr.
(McDonnell-Douglas Astronautics Co. Huntington Beach, CA, United States)
Johnson, R., Jr.
(McDonnell Douglas Astronautics Co. Huntington Beach, Calif., United States)
Dunn, T. J.
(NASA Johnson Space Center Houston, Tex., United States)
Date Acquired
August 9, 2013
Publication Date
September 1, 1979
Subject Category
Astronautics (General)
Report/Patent Number
IAF PAPER 79-106
Report Number: IAF PAPER 79-106
Accession Number
79A53298
Distribution Limits
Public
Copyright
Other

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