Rigidized Inflatable Veritex(TM) Structured For RF Antennas, Phase I
Data and Resources
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Rigidized Inflatable Veritex(TM) Structured...HTML
Techport Project Page
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Rigidized Inflatable Veritex(TM) Structured...HTML
Techport Project JSON Metadata
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Rigidized Inflatable Veritex(TM) Structured...HTML
Techport Project XML Metadata
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Rigidized Inflatable Veritex(TM) Structured...HTML
Techport Project PDF Export
| Field | Value |
|---|---|
| accessLevel | public |
| bureauCode | {026:00} |
| catalog_@context | https://project-open-data.cio.gov/v1.1/schema/catalog.jsonld |
| catalog_@id | https://data.nasa.gov/data.json |
| catalog_conformsTo | https://project-open-data.cio.gov/v1.1/schema |
| catalog_describedBy | https://project-open-data.cio.gov/v1.1/schema/catalog.json |
| identifier | TECHPORT_5179 |
| issued | 2005-07-01 |
| landingPage | https://techport.nasa.gov/view/5179 |
| modified | 2020-01-29 |
| programCode | {026:027} |
| publisher | Space Technology Mission Directorate |
| resource-type | Dataset |
| source_datajson_identifier | true |
| source_hash | 66ea9cf6efe854ee898066d0dd08e6b356aef29d |
| source_schema_version | 1.1 |
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| isopen | False |
| license_id | notspecified |
| license_title | License not specified |
| maintainer | TECHPORT SUPPORT |
| maintainer_email | hq-techport@mail.nasa.gov |
| metadata_created | 2025-11-21T21:21:21.322908 |
| metadata_modified | 2025-11-21T21:21:21.322912 |
| notes | Cornerstone Research Group inc. (CRG) proposes to demonstrate the feasibility of a lightweight, deployable Veritex <SUP>TM</SUP> supporting annulus structure to support large radio frequency (RF) antennas. Veritex<SUP>TM</SUP> composites are similar to other high-performance composites, with the exception 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 will develop and evaluate materials and related fabrication technologies based on Veritex<SUP>TM</SUP>, and develop a deployment scheme with built-in redundancy. 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 rigidized inflatable structures. |
| num_resources | 4 |
| num_tags | 10 |
| title | Rigidized Inflatable Veritex(TM) Structured For RF Antennas, Phase I |