Attachment_L-6,__Relevancy_Matrix.xlsx
XLSX spreadsheet 20 KB Posted
- Attached to
- Wind Tunnel Compressor Rotor Blades Federal contract opportunity
- Solicitation number
- FA9101-17-R-1000
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Atch L-6, Relevancy Matrix
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Sheet1
| Offeror: | Prime | Reference 1 | Reference 2 | Reference 3 | ||
| TECHNICAL CAPABILITIES | ||||||
| Design and Analysis Capability | ||||||
| D/A 1 | Use of 3D design software | |||||
| D/A 2 | Use of Finite Element Analysis software | |||||
| D/A 3 | Design of composite structures | |||||
| D/A 4 | Analysis of composite structures | |||||
| D/A 5 | Design of composite structures with a length >/= to 81 inches | |||||
| D/A 6 | Analysis of composite structures with a length >/= to 81 inches | |||||
| D/A 7 | Integration of design to properly interact with existing components | |||||
| D/A 8 | Design of composite rotor or compressor blades | |||||
| D/A 9 | Analysis and design to integrate composite compressor or rotor blades to properly interact with existing components | |||||
| D/A 10 | Design rotor blades with a length >/= to 81 inches | |||||
| D/A 11 | Analysis of rotor blades with a length >/= to 81 inches | |||||
| D/A 12 | Design of compressor blades with a length >/= to 81 inches | |||||
| D/A 13 | Analysis of compressor blades with a length >/= to 81 inches | |||||
| D/A 14 | Design of Compressor or rotor blades with cord length >/= to 22 inches | |||||
| D/A 15 | Analysis of Compressor or rotor blades with cord length >/= to 22 inches | |||||
| D/A 16 | Design of tooling for fiberglass/carbon fiber/hybrid composites | |||||
| D/A 17 | Design of tooling for fiberglass/carbon fiber/hybrid composites >/- 81 inches in length | |||||
| D/A 18 | Design of tooling made from composites, metal or hybrid materials | |||||
| D/A 19 | Analysis using composite structures utilizing composite failure criteria | |||||
| D/A 20 | Analysis using composites progressive failure analysis | |||||
| D/A 21 | Analysis of composites service life in fatigue and time | |||||
| Testing Approach | ||||||
| T 1 | Develop a composite test plan incorporating materials, components, and structures | |||||
| T 2 | Implement a composites test plan incorporating materials, components, and structures | |||||
| T 3 | Analysis of composite test results incorporating materials, components, and structures | |||||
| T 4 | Develop a composite repair plan | |||||
| T 5 | Develop a composite test plan of a rotor or compressor blade | |||||
| T 6 | Implement a composites test plan of a rotor or compressor blade | |||||
| T 7 | Analysis of composite test results of a rotor or compressor blade | |||||
| T 8 | Develop a composite repair plan for a rotor or compressor blade | |||||
| Manufacturing Capability | ||||||
| M 1 | Composite structures | |||||
| M 2 | Composite structures with a length >/= to 81 inches | |||||
| M 3 | Rotor blades | |||||
| M 4 | Rotor blades with a length >/= to 81 inches | |||||
| M 5 | Compressor blades | |||||
| M 6 | Compressor blades with a length >/= to 81 inches | |||||
| M 7 | Composite compressor blades | |||||
| M 8 | Composite compressor blades with a length >/= to 81 inches | |||||
| M 9 | Compressor or rotor blades with cord length >/= to 22 inches | |||||
| M 10 | Composite fabrication with fiberglass, carbon, hybrid materials | |||||
| M 11 | Composite tooling >/= 81 inches in length | |||||
| M 12 | Tooling for fiberglass/carbon fiber/hybrid rotor or compressor blades | |||||
| M 13 | Tooling for fiberglass/carbon fiber/hybrid rotor or compressor blades >/= 81 inches in length | |||||
| M 14 | Production run of a single composite structure design >/= 200 units | |||||
| M 15 | Production run of a single composite rotor or compressor blade design >/= 200 units | |||||
| Program Management | ||||||
| M-2.2.6.1. | Integrated Master Schedule | |||||
| M-2.2.6.2. | Configuration Management | |||||
| M-2.2.6.3. | Risk Management | |||||
| M-2.2.6.4. | Quality Control |
&"-,Bold"ATTACHMENT L-6 Relevancy Matrix Compressor Rotor Blades
FA9101-17-R-1000
Attachment L-6
File details come from the government source that posted it. Updated .