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Post by Obviousman on Dec 20, 2010 17:39:41 GMT -4
Hi! On this page: www.clavius.org/techexhaust.htmlYou report the DPS as being throttlable between 10% and 94%. Although your page refers to Apollo 12, both the Apollo 11 Press Kit and Apollo Experience Report: Mission Planning for the LM - Descent and Ascent say it was only throttlable up to about 60%. Can I get a double check on your figures?
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Post by Czero 101 on Dec 21, 2010 14:39:10 GMT -4
Hi! On this page: www.clavius.org/techexhaust.htmlYou report the DPS as being throttlable between 10% and 94%. Although your page refers to Apollo 12, both the Apollo 11 Press Kit and Apollo Experience Report: Mission Planning for the LM - Descent and Ascent say it was only throttlable up to about 60%. Can I get a double check on your figures? Lunar Module Handbook, Volume 1 page 2.1-35 (pdf page 76 "Throttle Control") lists the throttle range as 10% - 92.5%, however, a more detailed explanation on page 2.3-2 (pdf page 253 last paragraph) says the following: Paragraph 2.3.3.3.1 (pdf page 267) discusses the relationship between TTCA inputs and LGC throttle command outputs in the Automatic mode, the transition to Manual mode, and CMD THRUST (desired Commanded Thrust) and ENG THRUST (actual Engine Thrust) readouts. Cz
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Post by Obviousman on Dec 21, 2010 17:31:13 GMT -4
Thanks for that.
I'm wondering if it might need a little revision then, stating the normal throttle range and the contingency throttle range?
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Post by Czero 101 on Dec 22, 2010 5:27:54 GMT -4
Its not incorrect to say that the DPS was throttlable from 10% to 94%, just a little inaccurate, so perhaps a slight revision might be in order. I don't think its of very high priority, though.
Of course, it is still Jay's decision.
Cz
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