
Originally Posted by
Aaron Gustaveson
But you presented no "basic physics", just a number.
I did not say "linear velocity", I said "velocity". Which is, in this case, implicitly linear. But escape velocity has nothing to do with acceleration, so that part of your comment suggests some misunderstanding on your part.
As far as your argument that "Russian government would expose it" I think you are making some large assumptions about what a given government thinks, or why it does what it does. This is, again, an argument you hear all the time with respect to WTC-7. "If it was a controlled demolition, certainly someone would have come out and blown the whistle". In both cases the argument that "someone would expose it" when weighed again the massive amount of empirical evidence is a very weak argument. Not to mention that if the Russian government came out and said it was fake, you and nearly all Americans would not have believed it anyway.
As far as the physics, they are well beyond the scope of this thread, but I will give some links to help (assuming you are actually interested). If you are interested in the velocity required to escape the Moon's orbit, you can start here:
http://en.wikipedia.org/wiki/Escape_velocity
That link, and other source will consistently list the escape velocity of the Moon as 2400 meters per second (also note this is a measure of
velocity not acceleration. Acceleration would have been listed in meters per second per second m/sec/sec) This is because acceleration is a measure of the change in velocity over time.
In my original comment I said "basic physics". That was misleading. The physics is actually quite complicated. The details and explanation is well become the scope of this thread, not to mention typing the mathematical symbols required for summation and integration into a forum post would be difficult. If you are genuinely interested (and have not already made up your mind based on what you
want to believe) you can begin by learning to calculate delta-v. Also you need to understand specific impulse.
http://en.wikipedia.org/wiki/Delta-v
http://en.wikipedia.org/wiki/Specific_impulse
http://www.grc.nasa.gov/WWW/k-12/airplane/specimp.html (this one is going to be particularly important to you later)
This will give you a basis to understand Tsiolkovsky's equation. This equation, which far more primitive that what you need to actually launch a rocket, can help get you started in understanding the calculus involved.
http://en.wikipedia.org/wiki/Tsiolko...ocket_equation
At that point you will be ready to start double-checking the numbers listed by NASA for the ascent module, listed here a few pages down
http://en.wikipedia.org/wiki/Apollo_Lunar_Module
But we're still not there yet. From here we need to talk about rocket types, fuel, oxidizers, and their respective volumes, masses, and engine efficiency.
http://www.braeunig.us/space/propel.htm
That link will show you various liquid-fuel engines and their ISP, as well as the densities of various fuel types. You can cross-reference wikipedia to determine which types were used in the lunar ascent module.
After you have become fluent in all of these concepts we can do what wikipedia will not do, calculate the burn time. To do this, go back and refer to this page again:
http://www.braeunig.us/space/propuls.htm
in figure 1.21 you will see the equation used to determine burn-time.
Calculate that number, based on all the information NASA gives you. Then you also need the rate of fuel consumption, which is also conspicously missing from the NASA numbers. Some of the details are not available anywhere in fact, as they are a matter of national security. But using known controls you can take some educated guesses.
What you'll find is that you need a sustained burn of more than 10 minutes to come even close to the 2400 m/sec required. If you really do your homework you will also notice that achieving a stable orbit does not require the entire escape velocity, but is generally assumed to be about 71% of it. Since the force of gravity is reduced by the inverse-square of the distance, most of the velocity is required to get into orbit, with a small fraction required to go from a low-orbit to escape the system completely.
At this point we have to do the calculus, which I am not willing to do here. It's not my intention to try to convince you of anything. In fact I was reluctant to even type this response. In the end I chose to mainly because there may be some people reading it who have some background in math or physics who are open minded and actually interested in doing the math. So I'm trying to provide the resources you need to do so.