Self-Deploying Gossamer Support Structure, Phase II
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| Field | Value |
|---|---|
| Groups |
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| Tags |
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| isopen | False |
| license_id | us-pd |
| license_title | us-pd |
| maintainer | TECHPORT SUPPORT |
| maintainer_email | hq-techport@mail.nasa.gov |
| metadata_created | 2025-12-01T00:18:16.328742 |
| metadata_modified | 2025-12-01T00:18:16.328745 |
| notes | Phase I results demonstrated the feasibility of using shape memory polymer composites to deploy, tension and support gossamer antennas. Cornerstone Research Group, Inc. (CRG) has completed the critical initial development steps for a deployable support structure meeting NASA's requirements for a structure to deploy, tension, and support gossamer antennas. CRG proposes to further develop this lightweight, self-deploying Veritex<SUP>TM</SUP> strut for use as a supporting structure for gossamer antennas. Veritex<SUP>TM</SUP> composites are similar to other high-performance composites, except that CRG's shape memory polymer (SMP) resin, Veriflex<SUP>TM</SUP>, is used as the matrix resin. This allows for easy manipulation of the composite above the activation temperature, making it a unique material for use in dynamic structures and other applications requiring both load strength and "shape-shifting" modulus flexibility. In this Phase I program, CRG has developed and evaluated materials and related fabrication technologies based on Veritex<SUP>TM</SUP>, and produced a sub-scale working proto-type. This technical approach fulfills NASA's requirement for a very large, lightweight, on-orbit deployable RF antenna aperture structure by offering a practical, deployable, structural support that will address the short comings of current rigidified inflatables and mechanically deployed structures. |
| num_resources | 4 |
| num_tags | 8 |
| title | Self-Deploying Gossamer Support Structure, Phase II |