NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Composite lattice structureA lattice type structural panel concept which exploits the unidirectional character of filamentary advanced composite materials was described. This lattice has potential for applications where stiff lightweight structures are needed such as large area panels for space satellites. Formulae are presented to calculate the panel weight and plate bending stiffness. This analysis indicates that structures with significantly lighter weight than conventional minimum gauge sandwich construction can be fabricated. A suggested fabrication procedure is also presented along with photographs of some typical panels.
Document ID
19750024087
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Rhodes, M. D.
(NASA Langley Research Center Hampton, VA, United States)
Mikulas, M. M., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1975
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-X-72771
Report Number: NASA-TM-X-72771
Accession Number
75N32160
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available