Power System Electronics (PSE) Development for SmallSat Technology
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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_17380 |
| issued | 2016-09-01 |
| landingPage | https://techport.nasa.gov/view/17380 |
| modified | 2020-01-29 |
| programCode | {026:027} |
| publisher | Space Technology Mission Directorate |
| resource-type | Dataset |
| source_datajson_identifier | true |
| source_hash | f1677efe761752703209048f5b055e5baf79512e |
| source_schema_version | 1.1 |
| Groups |
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| Tags |
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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 | 2025-11-22T20:05:49.994904 |
| metadata_modified | 2025-11-22T20:05:49.994909 |
| notes | <p>We develop a modular Power System Electronics (PSE) that is reliable, efficient, and flexible to meet the Goddard Modular Smallsat Architecture (GMSA) challenge. With GSFC careful in-house design, we will have control over testing and manufacturing to produce a high quality, affordable PSE compatible with the Common Electronics Board (CEB), and be able to adapt interface and mechanical form factor that directly support NASA’s small satellite missions.</p> <p>To design and implement an in-house flight modular Power System Electronics (PSE) suitable for small satellite science missions; especially to support the Goddard Modular Smallsat Architecture (GMSA).</p><p>This research will have the following direct return on investment:</p><ul><li>In-house design reduces risk because we take control over all phases: design, parts selection, layout, assembly, integration and test, and tailor them to meet any unique science mission.</li><li>We first focus on circuit functionality to be tested with automotive EE components for smaller footprint, lower cost, and short lead time. In the meantime, we consider space-grade components as an optional recommendation for future missions which involved in a specific radiation environment. The risk will be reduced by validating the final architecture, performing the initial component market searches, testing candidate components, and demonstrating a working prototype board.</li></ul> |
| num_resources | 4 |
| num_tags | 10 |
| title | Power System Electronics (PSE) Development for SmallSat Technology |