Small Business Innovation Research/Small Business Tech Transfer
Integrated Variable Fidelity Conceptual Design, Phase I
Project Introduction
CADNexus proposes to develop an Integrated Variable Fidelity Conceptual Design tool. The application will enable design and analysis of unconventional and advanced concepts in the conceptual design phase. The application will be integrated not only in the conceptual design phase but throughout the entire design process from conceptual design, to preliminary design, to detailed design. The integration across design stages is accomplished by development of a component library that will store detailed aircraft shapes and components as well as rich metadata about the components, their attributes, and any other pertinent data. The library will enable designers to generate candidate design concepts given a set of mission requirements or other characteristics. In addition to performance analysis of a conceptual design the tool will also provide and evaluation of risk by projecting the probability that the design may not satisfy its mission requirements.
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Anticipated Benefits
Non-NASA Commercial Applications include geometry-centric conceptual design and risk analysis for products other than aircraft. We anticipate that automotive designers and other product designers find our tools highly beneficial. NASA has an ongoing need for conceptual design tools that are capable of performing multi-disciplinary analysis on unconventional or advanced concepts. Existing tools developed both within NASA and by commercial entities are not flexible enough to make this a reality. CADNexus proposes to leverage its existing core product and geometry-centric philosophy coupled with optimal estimation techniques applied to risk management into a commercial product offering. We envision expanding the scope of the effort to provide a geometry-centric underpinning to subsequent design stages thereby unifying the underlying geometry representation across conceptual, preliminary, and detailed design. The potentially provides a major advantage in that there are no lossy translations due to file format conversions and the usual need for geometry repair when exporting and importing geometry.
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Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
| CADNexus Inc. | Lead Organization | Industry | Burlington, Massachusetts |
Langley Research Center
(LaRC)
|
Supporting Organization | NASA Center | Hampton, Virginia |
Primary U.S. Work Locations
-
Massachusetts
-
Virginia
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Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Lead Organization:
- CADNexus Inc.
Responsible Program:
- Small Business Innovation Research/Small Business Tech Transfer
Project Management
Program Director:
Program Manager:
Principal Investigator:
Project Duration
Start: Feb 2011
End: Sep 2011
Technology Maturity (TRL)
| Start: | 2 |
| Current: | 3 |
| Estimated End: | 3 |
Applied Research
Development
Demo & Test
Technology Areas
Primary:
- TX15 Flight Vehicle Systems
- TX15.2 Flight Mechanics
- TX15.2.4 Modeling and Simulation for Flight
Target Destination
Earth
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This is a historic project that was completed before the creation of TechPort on October 1, 2012. Available data has been included. This record may contain less data than currently active projects.