Sword_Of_Truth
Penultimate Amazing
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- May 8, 2006
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And your point is...?
Satellite height and ranging.
If a satellite is 303 miles up, it can see and be seen for about 1,500 miles in either direction, 3,000 miles total, roughly the breadth of the Atlantic Ocean at its broadest, between the USA and North Africa.
The Pacific is much bigger, roughly 11,000 miles across where it is widest east to west at the equator. Near the International Dateline the Pacific is roughly 9,500 miles north to south. To see and be seen roughly 5,500 miles in either direction, equivalent to being able to range the Pacific Ocean, a satellite needs to be 18,900 miles above the surface of the Earth.
So by running through all of these considerations, especially as regards the Mighty Pacific, we are able to determine that the only way to satellite range and measure the transPacific breadth was by planting an LRRR on the moon. We couldn't do a satellite at 19,000 miles.
The moon was obviously the only way to go.
And your point is...?
Yeah, except for those pesky geostationary satellites like Syncom 2 and Syncom 3, launched in 1963, which, being geosynchronous, were around 22,500 miles above the surface of the Earth.
This is why, even today, communications with China are routed through a communications system on the moon.![]()
Another point.
If a satellite passes over Lick Observatory, it is hardly possible for someone to simultaneously range it from Japan if the satellite's orbit is low. The Japanese laser could not "see" the low flying satellite from such a, relative to Lick Observatory, westerly position. But if the moon is settled nicely over the Pacific ocean, one could range the moon from both banks and get a good measurement of the Pacific's distance.
Those are not the same type of satellites. My point was not that they could not get a satellite orbiting at 19,000 miles, they had no satellite mountable laser reflector at the time. There was no "satellite laser ranging" that existed at the time. This is why they must use the moon. It is easy to do. Surveyor VII did it no sweat. Easier then sending men up there and no reason to actually risk men in a mission like this. And if they did, get a satellite with mounted reflector up at 19,000 miles, it may well have been observable as such, a part of a weapons system.
Without getting bogged down in discussions of satellite technology, best way to think of this, best way because it is very much true, if you range a satellite at 20,000 miles from the earth with a ruby laser, everyone knows you are up to ocean measuring and ICBM targeting. It's obvious and undeniable. Better to at least pretend you are doing something else like ranging the moon. Especially if you can get people to swallow the notion it is a "peaceful" non military operation.
According to the minutely prepared plans of the Strategic Air Command, an impending Soviet attack would have prompted the missile siloes in North Dakota to open, and the ICBMs to arc towards Moscow and kindred targets. The four test launches actually attempted all failed, whereupon the SAC gave up testing. Was it badly designed equipment, human incompetence, defense contractor venality or conspiracy?
Without getting bogged down in discussions of satellite technology, best way to think of this, best way because it is very much true, if you range a satellite at 20,000 miles from the earth with a ruby laser, everyone knows you are up to ocean measuring and ICBM targeting. It's obvious and undeniable. Better to at least pretend you are doing something else like ranging the moon. Especially if you can get people to swallow the notion it is a "peaceful" non military operation.
HIDING THE BIRD
On page 5 of the Apollo 11 Mission Report's Section 5, we find the report's authors referring us to figure 5-3. In the second paragraph of the section quoted, the report's authors state there was a 20,000 foot down range error existing at the time of powered descent initiation.
Here is the relevant Mission Report citation;
"Figure 5-B contains histories of altitude compared with altitude- rate from the primary and abort guidance systems and from the Network powered flight processor. The altitude difference existing between the primary system and the Network at powered descent initiation can be ob- served in this figure. All three sources are initialized to the primary guidance state vector at powered descent initiation. The primary system, however, is updated by the landing radar, and the abort guidance system is not. As indicated in the figure, the altitude readouts from both systems gradually diverge so as to indicate a lower altitude for the primary system until the abort system was manually updated with altitude data from the primary system.
The powered flight processor data reflect both the altitude and downrange errors existing in the primary system at powered descent initiation. The radial velocity error is directly proportional to the downrange position error such that a 1000-foot downrange error will cause a 1-ft/sec radial velocity error. Therefore, the 20 000-foot downrange error existing at powered descent initiation was also reflected as a 20-ft/sec radial velocity residual. This error is apparent on the figure in the altitude region near 27 000 feet, where an error of approximately 20 ft/sec is evident. The primary-system altitude error in existence at powered descent initiation manifests itself at touchdown when the powered flight processor indicates a landing altitude below the lunar surface. Figure 5-4 contains a similar comparison of lateral velocity from the three sources. Again, the divergence noted in the final phases in the abort guidance system data was caused by a lack of radar updates."
Also, we note as a consequence, not only has a downrange error/adjustment become an issue, but a radial error of 20 feet per second must be taken into account. So the Eagle will not only land long, but also land left, or more precisely, land south of the originally targeted 0.731 north. Obviously, the Eagle cannot land if it is drifting south at 20 feet per second, it will break its legs off. But let's assume for the whole way down, the Eagle is drifting south 20 feet per second above and beyond the anticipated.