No, this is the same shell game you've been trying here all day without success. The claim you have retracted in this statement is the claim that a hoax best explains the LM ascent. That's not the same as retracting the claim that you have singlehandedly created a physically correct model that better explains it. If it is still your published belief that you have a physically correct model, then that is still on the table to be challenged here. If you don't want it challenged on the grounds that you no longer believe in its objective correctness, retract that.
My statement contained ample indications of "uncertainty".
To satisfy your demands, I've word smithed it to ensure uncertainty is expressed on every single statement, and even highlighted the fact that I am not a rocket scientist.
Anyone reading this is sure to know that I am not qualified nor claiming that my analysis is accurate.
It now reads:
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I have completed the Lunar Launch Speed analysis, and that was a long road to a personal conclusion that this MLH theory is possibly debunkable, based upon the inclusion of “Static Pressure Thrust”, which may be exceptionally high for the Ascent Launch with a platform directly beneath it. If so, then NASA may have modeled the acceleration reasonably well when they pulled it up by the cable.
This argument DOES NOT support the MLH theory, unless someone with deeper understanding of Rocket Engines can indicate that this setup of “high static pressure” wouldn’t be extraordinarily dangerous, or grossly interfere with the other forms of thrust (Momentum Thrust) as it reached the 0.5 meter point. This analysis is above my pay grade, so I will not be attempting any such analysis.
My initial analysis omitted the concept of Static Pressure Thrust, which could be HIGH at take-off. A re-analysis of 20 Frames of Apollo 16, with a thorough spreadsheet of intermediate results has revealed that it could be possible to explain the acceleration rate with the inclusion of Static Pressure Thrust, while also assuming that the rest of this rocket’s thrust is not reduced by too much.
In short, from the vantage point of a non-rocket-scientist, Static Pressure Thrust could potentially account for enough added boost during the first 0.5 seconds in order to give it the velocity to carry it through to the 1.8 meters high at 1.0 seconds into the flight.
Although personally, I still firmly believe the Human Moon Landings were faked, this particular analysis appears to hold little-to-no weight to this end. From what I can see, the actual Ascent Module specs/setup, could feasibly produce the acceleration curves witnessed in all 3 Lunar Launches - 15, 16, and 17.
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Teacher may I please be excused from this thread that I have conceded?