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As to what we saw and/or didn't see, as in other threads, I state once again that there was technology used we were not allowed knowledge of, and once again I question the validity of the radio transmissions from the moon. If one goes back to the originals, the normal voice channels were cut off after some statements by the astronauts, one asking "what the hell is that?" and another stating that something makes ours look like a horse and buggy, or something similar to that. Communications between the nauts and Houston was then patched coded through the physical monitoring channels.
What technology was it that we were not aware of?
"What the hell is that," was stated more than once during an Apollo mission (Apollo 12's launch, for one!). What transmissions are you talking about (identify mission, event, etc.)? I can supply the conversation in context and make its meaning clear. Ohterwise, there's no point in talking about transmissions.
"Patched coded through physical monitoring channnels..."?
Please show some substantiation for this contention.
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Some of the photography does not line up, which implies that it has been fooled with.
Please explain what this means as well. Examples, etc. (Identified, again). I have previously shown many times that there are no anomalies in Apollo photographs. There have been extensive threads regarding small snippets of video which are actually rather clear in what they show (to the knowledgable), and a lengthy, obtuse illustration of pareidolia regarding reflections in helmet visors.
I trust we're not going to delve into the unprovable again here?
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I would also like to see the mathematics regarding the capability of the lunar lander rocketry, and whether it was in fact capable of liftoff, so I would ask the thrust of the rocketry and the total mass of the lander/cargo, and the fuel available to make such a liftoff. There does seem to be some question about that.
Liftoff from the Moon?
Well, that's pretty simple stuff in principal. More thrust than weight lifted does the trick in a gravity field.
3500 pounds of thrust, 1650-1700 pounds of spacecraft (about 10000 pounds of mass). That implies about a 2 g push...up.
The engine was propelled by Dinitrogen Tetroxide and Aerozine 50, at a mixture ratio of approximately 1.6 (Oxidizer to Fuel). There were approximately 5200 pounds of propellant loaded in the Ascent Stage tanks (870 pounds lunar weight), which burned at a rate of ~11 lbs./sec. during an approximately 7.25 minute ascent burn.
About 90% of the APS propellant was consumed during this burn.
I don't think there's any question about this (at least there shouldn't be), as it is all published in detail for each Apollo mission, and has been since the mission reports were written. Given the voluminous nature of Apollo documentation, what question is there about this vehicles capabilities to do what it was designed to do...?