| TABLE OF CONTENTS |
| 1. | Electrical Requirements | 3 |
| 1.1. | Point to Point Connectivity | 3 |
| 1.2. | Current Requirements | 3 |
| 1.3. | High-Speed Signal Integrity | 3 |
| 1.4. | High Component Density | 3 |
| 1.5. | Terminations | 3 |
| 2. | Mechanical Requirements | 3 |
| 2.1. | Physical Size and Shape | 3 |
| 2.2. | Bending | 3 |
| 2.3. | Thermal Properties | 3 |
| 2.4. | Dimensional Stability | 3 |
| 2.5. | Dielectric Properties | 3 |
| 3. | Feature Interactions | 4 |
| 3.1. | Electrical Issues | 4 |
| 3.2. | Mechanical Issues | 4 |
| 4. | Balancing Demands | 6 |
| 4.1. | Micro-Strip Construction | 6 |
| 4.2. | Placement for Maximum Heat Dissipation | 6 |
| 4.3. | Cross-Hatching Plane Layers to Increase Flexibility | 7 |
| 4.4. | Replace Copper Planes with Flexible Conductive Coating | 7 |
| 4.5. | Unbonding Layers in Critical Areas | 8 |
| 4.6. | Selective Removal of Cover Material | 8 |
| 4.7. | Add a "pads-only" Layer | 8 |
| 4.8. | Heat-Form the Circuit | 8 |
| 4.9. | Employ Custom Tooling for Cold Forming | 8 |
| 4.10. | Know Your Termination Schemes before Designing the Circuit | 9 |
| 5. | Summary | 9 |
| 6. | Figures | |
| 6.1. | Selectively Bonded Layers Can Increase Flexibility in Critical Areas | 5 |
| 6.2. | Fully Bonded Construction | 5 |
| 6.3. | A Method Used in Rigid Flex Construction to Reduce or Eliminate the Amount of Acrylic Adhesive in Critcal Areas Is Called a Cut-Back or "bikini" Covers | 5 |
| 6.4. | The Use of Cross Hatch Plane Layers to Control EMI Can, in Some Cases, Increase Flexibility without Impairing Electrical Performance | 7 |
| 6.5. | Silver Epoxy Coatings are More flexible Than a Copper Plane | 7 |
| 6.6. | Unbonded Construction Allows Individual Substrates to Flex Independently | 8 |