Kalyan 4-25-08

5 Analysis were carried out as follows.

All of them with Carbon rods, No Hexcel sheet, No mylar sheet. Left hinge was constrained, right hinge was allowed to move along the back Plate length(x-axis) and front face of the nose plate was constrained.

• Wire Loads are 1512N on all the 4 hole areas

• Material Properties

Name of the Material	Young's Modulus (MPa)	Density ( )	Poisson's Ratio
Polyurethane	5/28/07	9/24/07	3/31/08
Aluminum: Drawing and Assembly Package	10/8/07	3/10/08	5/12/08
stainless steel	4/14/08	9/22/08	9/22/08
Carbon fiber	4/14/08	9/22/08	9/22/08

Case 1. No gravity

Figure 4.25.08.1: Total Deformation in analysis Case 1

The remaining pictures with X, Y, Z Deformations are available at Remaining pictures of Case_1

The analysis report is available at File:4 25 08 1.pdf

Case 2. Ideal case of gravity

Figure 4.25.08.2: Total Deformation in analysis Case 2

The remaining pictures with X, Y, Z Deformations are available at Remaining pictures of Case_2

The analysis report is available at File:4 25 08 2.pdf

Case 3. Chamber 3

Figure 4.25.08.3: Total Deformation in analysis Case 3

The remaining pictures with X, Y, Z Deformations are available at Remaining pictures of Case_3

The analysis report is available at File:4 25 08 3.pdf

Case 4. Chamber 4

Figure 4.25.08.4: Total Deformation in analysis Case 4

The remaining pictures with X, Y, Z Deformations are available at Remaining pictures of Case_4

The analysis report is available at File:4 25 08 4.pdf

Case 5. Chamber 5

Figure 4.25.08.5: Total Deformation in analysis Case 5

The remaining pictures with X, Y, Z Deformations are available at Remaining pictures of Case_5

The analysis report is available at File:4 25 08 5.pdf