Micro-size Precision Timing Unit for CubeSat Applications
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Micro-size Precision Timing Unit for CubeSat...HTML
Techport Project Page
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Micro-size Precision Timing Unit for CubeSat...HTML
Techport Project JSON Metadata
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Micro-size Precision Timing Unit for CubeSat...HTML
Techport Project XML Metadata
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Micro-size Precision Timing Unit for CubeSat...HTML
Techport Project PDF Export
| 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 | 2025-12-02T10:33:30.673774 |
| metadata_modified | 2025-12-02T10:33:30.673779 |
| notes | <p>We propose to design, develop, fabricate, and test a micro-size accurate timing unit that offers unprecedented frequency stability over a wide range of temperature. The proposed micro-size precision clocks will reduce thermal sensitivity and susceptibility to shock and acceleration. The new micro-size reference clocks will have wide applications for CubeSats and for NASA’s future instruments that require miniaturized timing units.</p> <p>The timing units used for space applications are based on quartz crystal resonators, which have a small temperature coefficient of elasticity (TCE), large size and incompatibility with electronic fabrication processes. The micro-size timing unit will use MEMS fabricated silicon resonators replace the quartz crystal resonators to develop a better precision timing unit for space applications. The new precision timing unit will have a wide temperature range and lower susceptibility to shock and acceleration. It can be integrated into the electronics, which will reduce the size and lower cost for NASA’s future instruments.</p> |
| num_resources | 4 |
| num_tags | 8 |
| title | Micro-size Precision Timing Unit for CubeSat Applications |