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30 Jul 2002: A physicalmodel is built to analyse the feasibility of the concept and to test various deploy-ment schemes. ... A physicalmodel is built to analyse the feasibility of the concept and to test various deploymentschemes.

29 Feb 2000: Values ranged from 0.87 in test A2 to 1.33 in test C2, with the range being between 1.04 and 1.33 for the first 11 tests. ... Hudson tests. Kite tests. Collins tests. Antill tests. Test No. H1.

21 Jul 1998: Several tests were carried out on this one-way actuator, both in the one-disk and three disk configurations. ... Working torques used in the test varied from -0.2 Nm to 0.62 Nm.

17 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.

7 Jul 2004: The measurements from two nominally identical tests, both beginning with the rotation set. ... root hinge has significant curvatures both near the clamps and in the middle.

11 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.

21 Jan 2002: A summary of allthe test results and analytical predictions is given in Table 1. ... The test results for the overall stiffness of thehinge in each component direction can be seen in Figure 7.

18 Feb 2002: Theexperimental results presented in this reference are avery valuable benchmark against which to test new so-lutions. ... Comparison with Sewall’s Experiment. The third test case was based on one of the tests re-ported in Ref.

29 Mar 2004: The tests were done with a cross-head speed of5 mm/min, and were recorded with a Sony DCR-PC110E digital video camera. ... Displacement (mm). Fo. rce. (N. ). Test. Abaqus. 6. Fig. 17 Response to vertical tip loads.

23 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.

27 Aug 2002: Simple equilibrium considerations lead torelationships between the tension in the middle of cord i, Ti, the sag of cord i, si, and the sag of cord i 1,si1, etc. ... This was probably due to the damage mentioned above. This test confirmed a conclusion

14 May 2002: Simple equilibriumconsiderations lead to relationships between the tension inthe middle of cord i, Ti, the sag of cord i, si, and the sagof cord i 1, si1, etc. ... This test confirmed a conclusion already reached bySeffen et al. (2000), that an advantage

22 Mar 2002: thickness of the membrane. Values between 1% and100% of the thickness have been used, considering dif-ferent imperfection magnitudes to test the sensitivityof the predicted response. ... Note that all of these modes closely resemble theexpected wrinkled

12 Jul 2002: To cross-head. To baseof Instron. Figure 5.2: Kxx test set-up. Prediction of Rolamite Stiffness. ... ess. N/m. m2. E=13200. Figure 5.10: Stiffness test on coated wire used in hinge.

17 May 2005: Packaging. Displacement controlled static packaging tests werecarried out vertically in an INSTRON testing machine. ... Fig. 14 Localization of deformation in the verticalpackaging test. The finite element simulation results for Config VIII–

21 Mar 2001: 5 Packaging and Deployment Tests 345.1 Zig-Zag Folding. 365.2 Wrapping. 375.3 Folding Machine. ... Figure 4.7: Hub connection between hub and membrane. Chapter 5. Packaging and Deployment Tests.

14 Feb 2003: Twotypes of vibration tests were carried out: (i) a linearidentification test using slow sine sweep and constantsine excitation, and (ii) a nonlinear identification testusing slow sine sweep excitation. ... A Polytec PSV300scanning laser vibrometer was

21 Mar 2001: 293.10 Unstressed rib shape. 31. 4.1 Schematic top view of test article. ... 404.9 Schematic layout of tension test on membrane strip. 434.10 Tension tests on membrane strips.

28 Feb 2003: the bottombase. The middle module is rotated counter-clockwise through the same angle. ... To test the manufacturing and deployment procedures,four demonstrator masts were built at various stages inthe development process.

12 Nov 2003: These systems can host test structures ofalmost unlimited size even when motion exists. ... disadvantage.However, the range of possible dimensions of test articles is almost unlimited.

23 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