Vapor Chamber with Phase Change Material-based Wick Structure for Thermal Control of Manned Spacecraft, Phase I
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| 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_18486 |
| issued | 2014-12-01 |
| landingPage | https://techport.nasa.gov/view/18486 |
| modified | 2020-01-29 |
| programCode | {026:027} |
| publisher | Space Technology Mission Directorate |
| resource-type | Dataset |
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| license_id | notspecified |
| license_title | License not specified |
| maintainer | TECHPORT SUPPORT |
| maintainer_email | hq-techport@mail.nasa.gov |
| metadata_created | 2025-11-22T22:03:25.545789 |
| metadata_modified | 2025-11-22T22:03:25.545793 |
| notes | In response to NASA SBIR solicitation H3.01 "Thermal Control for Future Human Exploration", Advanced Cooling Technologies, Inc. (ACT) is proposing a novel Phase Change Material (PCM) vapor chamber to ameliorate the temperature fluctuations encountered during planetary (or lunar) orbit. The PCM vapor chamber will consist of a packed bed of micro-encapsulated PCM beads surrounded by a two-phase working fluid. The PCM beads will act as both a highly efficient thermal storage medium, as well as a wick structure for capillary pumping of the two-phase working fluid. The two-phase heat transfer by the working fluid increases the effective thermal conductivity of the PCM by a factor of 1000 or more. This approach eliminates the need for embedding thermally conductive metal fins or carbon foam, which typically consume at least 50% of the system mass in traditional PCM heat exchangers. The PCM vapor chamber not only has the potential to exceed a 2/3 PCM mass ratio using paraffin wax, but also provides several advantages over the state-of-the-art, water-based PCM heat exchangers. The concept proposed by ACT will eliminate the need for metal fins and foams, and significantly reduce the mass of non-PCM materials. In addition, the PCM vapor chamber can serve as either a stand-alone thermal capacitor or a dual thermal capacitor/heat exchanger. |
| num_resources | 4 |
| num_tags | 10 |
| title | Vapor Chamber with Phase Change Material-based Wick Structure for Thermal Control of Manned Spacecraft, Phase I |