1. Date of download: 6/1/2016 Copyright © 2016 SPIE. All rights reserved. Graphical and tabular representation of out-of-plane gravitational sag results for suggested thin mirror laminates. In the notation “x+ymm,” x is the CFRP skin thickness and y that of the honeycomb core. Figure Legend: From: Prototype carbon fiber composite deformable mirror Opt. Eng. 2007;46(9):094003-094003-7. doi:10.1117/1.2779337

2. Date of download: 6/1/2016 Copyright © 2016 SPIE. All rights reserved. FEA model of the predicted active mirror response on application of 10N to the central actuator. The edge actuators and flexures are modeled with beam elements. Figure Legend: From: Prototype carbon fiber composite deformable mirror Opt. Eng. 2007;46(9):094003-094003-7. doi:10.1117/1.2779337

3. Date of download: 6/1/2016 Copyright © 2016 SPIE. All rights reserved. Interferogram of the active mirror final surface after grinding and polishing, prior to assembly. Figure Legend: From: Prototype carbon fiber composite deformable mirror Opt. Eng. 2007;46(9):094003-094003-7. doi:10.1117/1.2779337

4. Date of download: 6/1/2016 Copyright © 2016 SPIE. All rights reserved. Picture of the assembled active mirror system with the nickel-coated CFRP faceplate. Figure Legend: From: Prototype carbon fiber composite deformable mirror Opt. Eng. 2007;46(9):094003-094003-7. doi:10.1117/1.2779337

5. Date of download: 6/1/2016 Copyright © 2016 SPIE. All rights reserved. Interferogram of measured (top) central and (bottom) edge influence functions showing the mirror shape on actuation with a central and edge actuator. A reference surface has been subtracted from these frames. Figure Legend: From: Prototype carbon fiber composite deformable mirror Opt. Eng. 2007;46(9):094003-094003-7. doi:10.1117/1.2779337

6. Date of download: 6/1/2016 Copyright © 2016 SPIE. All rights reserved. Comparison of measured and modeled influence function shapes. Figure Legend: From: Prototype carbon fiber composite deformable mirror Opt. Eng. 2007;46(9):094003-094003-7. doi:10.1117/1.2779337

7. Date of download: 6/1/2016 Copyright © 2016 SPIE. All rights reserved. Surface measurement of the mirror in its flattened position. The form error is 1.87μmrms. Figure Legend: From: Prototype carbon fiber composite deformable mirror Opt. Eng. 2007;46(9):094003-094003-7. doi:10.1117/1.2779337