Timeline for How did sloshing prevent the Apollo Service Module from moving safely away from the Command Module and how was this fixed?
Current License: CC BY-SA 4.0
8 events
| when toggle format | what | by | license | comment | |
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| Jul 7, 2019 at 22:51 | vote | accept | uhoh | ||
| Jul 1, 2019 at 15:16 | history | edited | Russell Borogove | CC BY-SA 4.0 |
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| Jul 1, 2019 at 14:50 | history | edited | Russell Borogove | CC BY-SA 4.0 |
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| Jul 1, 2019 at 3:34 | history | edited | Russell Borogove | CC BY-SA 4.0 |
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| Jul 1, 2019 at 3:28 | comment | added | Russell Borogove | The last diagram in the anomaly report appears to show a 25-second timer being added for the -X RCS shutoff, and the 5.3 second roll timer changed to 2 seconds, and I think those were hardware circuits, but the more extensive changes in your diagram were those made in response to the Apollo 13 anomalies: a backup oxygen tank for the fuel cells, a backup battery, and other belt-and-suspenders fixes, not related to the service module separation anomaly. | |
| Jul 1, 2019 at 3:22 | comment | added | uhoh | So the fix was primarily in timing/sequencing, or where there also hardware modifications (possibly described in the figure) that addressed this problem as well? | |
| Jul 1, 2019 at 3:20 | history | edited | Russell Borogove | CC BY-SA 4.0 |
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| Jul 1, 2019 at 3:05 | history | answered | Russell Borogove | CC BY-SA 4.0 |