File:AB5-K8mod.jpg
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Summary
| Description |
English: Cutaway drawing of the AB5-K8 gyro.
The ST-124 carried three of these gyros. Note the three mutually orthogonal axes that characterize the gyro's performance: spin (10), input (14) and output (6). The gyro is only sensitive to rotations around the input axis, and responds by precessing around the output axis. In the figure, the gyro has experienced some input rotation about axis 14, so the rotor has precessed through the angle 11, to point along direction 12. The angle 11 is proportional to the magnitude of the input rotation about 14. |
| Date | |
| Source | “Astrionics System Handbook for Saturn Launch Vehicles.” MSFC No. IV-4-401-1. IBM No. 68-966-0002., 1 November 1968. Figure 14.8-2 |
| Author | NASA |
Licensing
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This work is in the public domain in the United States because it is a work prepared by an officer or employee of the United States Government as part of that person’s official duties under the terms of Title 17, Chapter 1, Section 105 of the US Code.
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Original upload log
The original description page was here. All following user names refer to en.wikipedia.
- 2007-06-15 22:37 EdgarDurbin 720×886×8 (226146 bytes) Cutaway drawing of the AB5-K8 gyro. The ST-124 carried three of these gyros. Note the the three mutuall y orthogonal axes that characterize the gyro?s performance: spin (10), input (14) and output (6). The gyro is only sensitive to rotations around the
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 04:32, 26 March 2008 | | 720 × 886 (221 KB) | File Upload Bot (Magnus Manske) | {{BotMoveToCommons|en.wikipedia}} {{Information |Description={{en|Cutaway drawing of the AB5-K8 gyro. The ST-124 carried three of these gyros. Note the the three mutuall y orthogonal axes that characterize the gyro?s performance: spin (10), input (14) an |
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