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NEW CONCEPTS FOR SPACECRAFT ANTENNAS AND RADAR STRUCTURESBASED ON ...
www-civ.eng.cam.ac.uk/dsl/publications/New%20concepts.pdf17 Feb 2006: Displacement (mm). Fo. rce. (N. ). Test. Abaqus. Figure 12: Response to horizontal tip loads. ... Displacement (mm). Fo. rce. (N. ). Test. Abaqus. 6. Figure 13: Response to vertical tip loads. -
Tape Spring Large Deployable Antenna
www-civ.eng.cam.ac.uk/dsl/publications/AIAA-2006-1601-386.pdf11 May 2006: TOP SIDE. Figure 11. Test piece drawing (dimensions in mm). 7 of 12. ... First test-piece (a) hung for display (b) showing connectors at the back. -
Wrinkled membranesPart I: experiments
www-civ.eng.cam.ac.uk/dsl/publications/jomms-v1-n1-p02-p.pdf23 Feb 2006: All test results presented in this section were obtained on 380 mm widemembranes with a height, between the supports, of 128 mm. ... Laser scanning frame. 3.2. Shear test apparatus. 3.3. Square membrane apparatus. -
Wrinkled membranesPart III: numerical simulations
www-civ.eng.cam.ac.uk/dsl/publications/jomms-v1-n1-p04-p.pdf23 Feb 2006: 5.1.1. Initial imperfections. Many different combinations of eigenmodes and scal-ing factors were considered to test the sensitivity of the results of the detailedwrinkling analysis. ... Because the wrinkles can most easily reorganise themselves in the
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