It looks like you're using an Ad Blocker.
Please white-list or disable AboveTopSecret.com in your ad-blocking tool.
Thank you.
Some features of ATS will be disabled while you continue to use an ad-blocker.
originally posted by: InfiniteTrinity
a reply to: neutronflux
Whats the matter? Can you point out what you disagree with?
Fine. Tell that to the other car when it hits the car in front of it.
Toward Earth's center, but that acceleration is counteracted by the satellite's momentum, the result is an orbit.
originally posted by: InfiniteTrinity
a reply to: neutronflux
So straight down then?
How does it maintain its speed to maintain the curved trajectory through space then?
Go ahead.
science.howstuffworks.com...
Orbital Velocity and Altitude
PREVNEXT
A rocket must accelerate to at least 25,039 mph (40,320 kph) to completely escape Earth's gravity and fly off into space (for more on escape velocity, visit this article at NASA).
Earth's escape velocity is much greater than what's required to place an Earth satellite in orbit. With satellites, the object is not to escape Earth's gravity, but to balance it. Orbital velocity is the velocity needed to achieve balance between gravity's pull on the satellite and the inertia of the satellite's motion -- the satellite's tendency to keep going. This is approximately 17,000 mph (27,359 kph) at an altitude of 150 miles (242 kilometers). Without gravity, the satellite's inertia would carry it off into space. Even with gravity, if the intended satellite goes too fast, it will eventually fly away. On the other hand, if the satellite goes too slowly, gravity will pull it back to Earth. At the correct orbital velocity, gravity exactly balances the satellite's inertia, pulling down toward Earth's center just enough to keep the path of the satellite curving like Earth's curved surface, rather than flying off in a straight line.
The orbital velocity of the satellite depends on its altitude above Earth. The nearer to Earth, the faster the required orbital velocity. At an altitude of 124 miles (200 kilometers), the required orbital velocity is a little more than 17,000 mph (about 27,400 kph). To maintain an orbit that is 22,223 miles (35,786 kilometers) above Earth, the satellite must orbit at a speed of about 7,000 mph (11,300 kph). That orbital speed and distance permit the satellite to make one revolution in 24 hours. Since Earth also rotates once in 24 hours, a satellite at 22,223 miles altitude stays in a fixed position relative to a point on Earth's surface. Because the satellite stays right over the same spot all the time, this kind of orbit is called "geostationary." Geostationary orbits are ideal for weather satellites and communications satellites.
You ever state a clear and concise argument why you think geostationary /geosynchronous satellites do not have angular momentum when using the earth’s axis as a point of origin?
From the launch vehicle that placed it orbit like any other satellite. Except for correction thrust from a limited supply of fuel?
Random example that has nothing to with this discussion.
I've explained that.
How does it maintain it speed to maintain its trajectory through space if its in fact being pulled down by gravity,
Satellites don't give a damn about Earth's rotation.
You see Phage, the other satellites have to fall around curvature to maintain a curved trajectory through space.
Actually it does, since the discussion involves momentum.
I've explained that.
Satellites don't give a damn about Earth's rotation.
You see Phage, the other satellites have to fall around curvature to maintain a curved trajectory through space.
originally posted by: InfiniteTrinity
a reply to: neutronflux
You ever state a clear and concise argument why you think geostationary /geosynchronous satellites do not have angular momentum when using the earth’s axis as a point of origin?
I didnt make that claim.
Also discussion still about stationary sats. You still dont know the difference?
If you are in a car moving at 20 mph and a car next to you is moving at 20 mph, does that mean the car next to you has no momentum?
How does it maintain it speed to maintain its trajectory through space if its in fact being pulled down by gravity.
How Satellites Stay in Orbit
www.universetoday.com...
So really, a satellites ability to maintain its orbit comes down to a balance between two factors: its velocity (or the speed at which it would travel in a straight line), and the gravitational pull between the satellite and the planet it orbits. The higher the orbit, the less velocity is required. The nearer the orbit, the faster it must move to ensure that it does not fall back to Earth.
After fighting a losing battle against gravity, the European Space Agency's GOCE satellite has made splashdown somewhere in the south Atlantic Ocean, says the ESA.
www.csmonitor.com...!-Falling-GOCE-satellite-lands-in-the-Atlantic
You seemed to think that because a geostationary satellite does not move relative to Earth's surface it has no momentum. This is incorrect. I used an example (not random) to illustrate this.
I see so any random example involving momentum applies.
Its speed is maintained because it is determined by the resultant vector of gravity and the satellite's momentum. The forces balance, the speed doesn't change.
Can you explain it again cause I cant find it.
Your whole argument is based on the fact that an object in geostationary orbit has an angular velocity which matches Earth's rotation.
I didnt make an argument about Earth rotation.
So really, a satellites ability to maintain its orbit comes down to a balance between two factors: its velocity (or the speed at which it would travel in a straight line), and the gravitational pull between the satellite and the planet it orbits.
And satellites don’t always win the battle between forces....
I didnt claim they that have no angular momentum
The only correct frame of reference is the object Earth. In this frame of reference there is no angular momentum for the geostationary sat.
www.abovetopsecret.com...
How does it maintain its curved trajectory through space. An object has to fall around curvature to do that.
www.abovetopsecret.com...
Because you cannot explain how it maintains a curved trajectory through space. You can keep posting those numbers like they mean anything but you have to explain HOW IT IS POSSIBLE that it keeps flying in this curved trajectory through space with a speed of 1.91 mi/s, 22,236 mi above a point on the equator.
Geostationary orbits debunked.
www.abovetopsecret.com...
Since it doesnt fall around the Earth, which would maintain its velocity?
Can you now explain how a geostationary sat does it? Since it doesnt fall around the Earth, which would maintain its velocity?
You guys are hilarious. You keep posting the same dumb contradiction I debunked about 40 times now.
What is gravity?
spaceplace.nasa.gov...
Geostationary orbit
en.m.wikipedia.org...
A geostationary orbit, often referred to as a geosynchronous equatorial orbit[1] (GEO), is a circular geosynchronous orbit 35,786 km (22,236 mi) above Earth's equator and following the direction of Earth's rotation. An object in such an orbit appears motionless, at a fixed position in the sky, to ground observers. Communications satellites and weather satellites are often placed in geostationary orbits, so that the satellite antennas (located on Earth) that communicate with them do not have to rotate to track them, but can be pointed permanently at the position in the sky where the satellites are located. Using this characteristic, ocean-color monitoring satellites with visible and near-infrared light sensors (e.g. GOCI) can also be operated in geostationary orbit in order to monitor sensitive changes of ocean environments.
originally posted by: InfiniteTrinity
a reply to: neutronflux
I said,
In this frame of reference
Try to read.
You seemed to think that because a geostationary satellite does not move relative to Earth's surface it has no momentum.
Its speed is maintained because it is determined by the resultant vector of gravity and the satellite's momentum. The forces balance, the speed doesn't change.
Your whole argument is based on the fact that an object in geostationary orbit has an angular velocity which matches Earth's rotation.
You see Phage, the other satellites have to fall around curvature to maintain a curved trajectory through space.
Again, a satellite could care less at what speed the earth rotates.