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SI-C inboard engine shutdown
Did the inboard engine on the SI-C shut down on all flights? This PDF
http://www.klabs.org/history/reports...1970023342.pdf figure 2 doesn't show a drop in acceleration for the SI-C (as it does for the S-II). -- Replace you know what by j to email |
#2
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SI-C inboard engine shutdown
On Tue, 04 Aug 2009 15:02:37 -0400, Jud McCranie
wrote: Did the inboard engine on the SI-C shut down on all flights? This PDF http://www.klabs.org/history/reports...1970023342.pdf figure 2 doesn't show a drop in acceleration for the SI-C (as it does for the S-II). And it shows a max of about 4.5 Gs whereas the manned missions had about 3.9. -- Replace you know what by j to email |
#3
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SI-C inboard engine shutdown
In article ,
Jud McCranie wrote: On Tue, 04 Aug 2009 15:02:37 -0400, Jud McCranie wrote: Did the inboard engine on the SI-C shut down on all flights? This PDF http://www.klabs.org/history/reports...1970023342.pdf figure 2 doesn't show a drop in acceleration for the SI-C (as it does for the S-II). And it shows a max of about 4.5 Gs whereas the manned missions had about 3.9. The center engine was shut down to prevent "pogo" effect, where the acceleration and vibration created extra pressure head in the propellant, resulting in extra thrust and structural resonance at approximately 1 Hz, which is harmful to humans aboard. This phenomenon was discovered in the first (unmanned) flight; shutdown times were varied so as to reduce pogo. -- Remove _'s from email address to talk to me. |
#4
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SI-C inboard engine shutdown
On Tue, 04 Aug 2009 23:50:34 -0400, Orval Fairbairn
wrote: This phenomenon was discovered in the first (unmanned) flight; shutdown times were varied so as to reduce pogo. Actually it was the second Sat V (Apollo 6) that had the pogo, so that chart must have been from A4 or A6. -- Replace you know what by j to email |
#5
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SI-C inboard engine shutdown
Orval Fairbairn wrote:
The center engine was shut down to prevent "pogo" effect, where the acceleration and vibration created extra pressure head in the propellant, resulting in extra thrust and structural resonance at approximately 1 Hz, which is harmful to humans aboard. It's not just that it's harmful to humans at that particular frequency, it's that pogo (whose frequency varies with vehicle) is high amplitude and thus potentially damaging to structure and systems. D. -- Touch-twice life. Eat. Drink. Laugh. http://derekl1963.livejournal.com/ -Resolved: To be more temperate in my postings. Oct 5th, 2004 JDL |
#6
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SI-C inboard engine shutdown
"Derek Lyons" wrote:
The center engine was shut down to prevent "pogo" effect, where the acceleration and vibration created extra pressure head in the propellant, resulting in extra thrust and structural resonance at approximately 1 Hz, which is harmful to humans aboard. It's not just that it's harmful to humans at that particular frequency, it's that pogo (whose frequency varies with vehicle) is high amplitude and thus potentially damaging to structure and systems. On Apollo 6, it actually caused some of the outer laminated material covering the conical Lunar Module adapter between the third stage and the command/service module to sheer away from the launch vehicle. They were very close to a total structural failure on the SLA during that launch due to pogo. T.B. |
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