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Rene-NASA-Mooned-America

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Gotchas ! / Chap. 17 p. 152<br />

high speed. Just as you must apply the brakes while coming down a hill to round a sharp<br />

curve, the service engine must deaccelerate the space craft as they zipped down the Moon's<br />

gravity hill in order to make the turn around the Moon.<br />

Well these men had "The Right Stuff, and had already begun to implement their sensible<br />

retreat to the LEM while mission control was still dithering and blathering. 20 Mission control<br />

finally agreed to allow them to use the LEM's decent engine to enter a lunar orbit and again<br />

to blast for Earth. This also meant that any necessary mid-course corrections would also<br />

depend solely on the LEM's 9 tons of fuel. Adding to the equation is the fact that, in addition<br />

to the 20 or so tons of unburned fuel in the service vehicle there would be an additional<br />

15,400 pounds of LEM, plus its 9- tons of fuel plus 33,000 lbs for the service vehicle. That's<br />

over 100,000 pounds.<br />

When the service engine performs the same job, Aldrin, says the lunar orbit burn takes 6<br />

minutes. 21 Then Aldrin reports that, to send the craft back to Earth, it took a 2.5 minute burn<br />

which consumed 5-tons of fuel. 22 This is a rate of 2 tons per minute and indicates that the<br />

lunar orbit burn consumed 12 tons of fuel. Please bear in mind that the service engine has no<br />

throttle. It's either all on or all off. When operating, the engine consumes the maximum fuel<br />

per minute. This leaves us with the unalterable fact that 17 tons of fuel were needed to do the<br />

job, without any later mid-course corrections and without all that extra mass.<br />

And naturally, because of all the extra mass, it would logically have required much more<br />

than 5 tons of fuel to accelerate up the Moon's gravity hill for the return to Earth. Still ... the<br />

LEM only had 9 tons of fuel.<br />

They didn't even complete the first burn, yet, they were short 3 tons of fuel. <strong>NASA</strong><br />

would later claim that, "On the first three lunar flights, Apollos 8, 10, and 11, the spacecraft<br />

had been programmed so that the final engine burn launched the ship into a "free return<br />

trajectory". Once the craft looped around the moon, it would be on the correct course for its<br />

return trip to earth. No additional engine firings would be required." 23 This is suposedly a<br />

trajectory that doesn't require any lunar deacceleration to round the Moon and return directly<br />

to Earth.<br />

I am having a problem with <strong>NASA</strong>'s analysis. To get to the Moon you must travel away<br />

from the Earth. If you skim by the Moon you are still going away from the Earth. If your<br />

velocity is high you will then go a damn long way past the Moon before you will lose all<br />

velocity and then be sucked back toward it. Falling back will take as long as going out did.<br />

Apollo 13 didn't spend any extra days in space so how the hell did they rub off all that<br />

velocity<br />

Harry Hurt, the author of FOR ALL MANKIND is a most meticulous researcher and the<br />

following was in his book which was published in 1988. "The first burn would sling<br />

shot the spacecraft around the backside. The second and even more critical burn was the<br />

Trans-Earth Injection or TEI, which would blast the spacecraft toward home."<br />

24<br />

This is directly contradicted by THE FLIGHT THAT FAILED by Cooper which was<br />

<strong>NASA</strong> MOONED AMERICA! / <strong>Rene</strong>

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