alright1234
New Member
Does anyone know the sensitivity of the Parkes radio antenna and the units?
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I did a little calculation here. Do the values used seem responsible?
The power of the radio signal produce by the lander is estimated at 50 Watts. A radio signal's intensity is dependent on the inverse of the second order of the distance I = U2 = {[A cos(kr)]/r]}2 where A represents the power of the radio signal. After a radio signal propagates the distance of 238,000 miles (3.8 x 108 m) to the earth, a 50 W radio signal would diminish to I = A2 [cos2(kr)]/r2 = (50 W)2 (0.5) / (3.8 x 108 m)2 = 8.65 x 10-15 W2/m2. The Parkes large hyperbolic radio antenna located in Sydney Australia is used to communicate with the Apollo 11 mission. The sensitivity of the Parkes large hyperbolic radio antenna is extrapolated using the power of a 300 km height satellite that emits a 20 W radio signal that forms a detectable intensity at the surface of the earth I = A2 [cos2(kr)]/r2 = (20 W)2 (.5) / (3 x 105m)2 = 2.22 X 10-9 W2/m2. Adding two orders of magnitude to the satellite's power at the surface of the earth, the sensitivity of the Parkes radio antenna is estimated at 10-11 W2/m2. There is a four order of magnitude between the sensitivity of the Parkes and the 10-15 W2 /m2 s-band radio signal that originates from the Apollo 11 mission which suggest that NASA Apollo 11 lunar mission was hoax. Also, a radio signal cannot penetrate the Van Allen radiation belt that surrounds the earth. It is questionable how NASA communicated with the Apollo missions, Voyagers, and Mars probes using radio waves. It is argue that a satellite that is orbiting the earth at a height of 30,000 km above the earth that is passed the Van Allen belt justifies the functionality of the Apollo 11 communication system but the described satellite height is 10 % of the distance to the moon which is a doubtful magnitude for the height for orbiting communication satellite since there is no reason that a communication satellite would orbit at that height that would require more power to produce a usable signal at the earth. The space stations are orbiting the earth at the height of 130-250 miles above the earth. I predict that the maximum orbital height of a satellite is 500 miles.
I predict that the maximum orbital height of a satellite is 500 miles.
Sorry, total nonsense.I did a little calculation here. Do the values used seem responsible?
The antenna in a cell phone is not very efficient, usually just a slab of ceramic which has been metalised.A cell phone has the power of about 1 W and a range of 1 mile. How can a 50 W radio wave from the moon that is 238,000 miles from the earth form a detectable signal?
Probably because you do not know enough about radio stuff yet.It just does not make sense to me
That never seems to slow down the science deniers....Probably because you do not know enough about radio stuff yet...
Easily. The transmitter on Voyager I is only 22W, and NASA can receive its signal from 22 Billion km out in space, beyond the edge of our planetary system.Can a large radio telescope detect a 1 W cell phone signal 100 miles away?
So am I trying to discuss factual data with someone who doesn't believe we landed on the moon and that the Earth is flat?Straight up is difficult to determine since we have to rely on the integrity of NASA which I am contesting.
Can a large radio telescope detect a 1 W cell phone signal 100 miles away?
Again, nonsense.A cell phone has the power of about 1 W and a range of 1 mile.
Why can not a cell phone work from china to the USA or from Paris to NY without a tower?