Brock said:
When it's pushed in it gains PE because it's under pressure, when the pressure is released it loses energy by slowing down and moving out to a relaxed orbit. The professor is saying that it loses energy, moves in, and picks up velocity, well to pick-up v it must be forced in, in which case it would aslo pick up energy. So if it picks up v it does not lose energy like he said, unless it loses much energy falls in a closer orbit, and then gains a bit of pressure energy that pushed it in some to pick up v.
Okay, this is wrong for several reasons. First of all, pressure, which is force per unit area, has no relevance here; I'll assume you mean a force. Next, if you apply a force to reduce the radius of the orbit, you don't gain potential energy. You're thinking of pushing against some kind of restoring force as if there's a potential field associated with it, but that applies only to conservative forces. The "force" you "push" against in this case is the inertial centrifugal force, which is not a conservative force at all. In other words, even if you could simply "push" on an orbiting object to get it "move in", you could not get back the work you did in the way you can with a conservative force field, so you don't gain potential energy.
Last, the way you reduce the radius of a circular orbit is to apply a force in the negative velocity direction, which slows down the orbiting object, reducing its kinetic energy. (Actually, you do it twice - once to convert to an elliptical orbit with perigee at the lower radius and apogee at the original radius, and then again at the perigee location to lower the apogee to the new radius, converting to a circular orbit again - it's called a "Hohmann Transfer" if you want to look it up.) Although you've slowed down the object with the application of the first force (which is why it now follows a lower trajectory than before), it still speeds up as it falls, so that its velocity at perigee is higher than the original velocity. After the second application of force, the velocity at perigee is reduced so that the object now follows a lower trajectory and doesn't reach the prior apogee height. Its energy is now lower than what it started with, but its velocity is higher because that's true for any circular orbit with a smaller radius - Kepler's Third Law.
Brock said:
In the case of planets is mass the only thing that determines how fast an object travels as it orbits another?
Nope - go back to your basic lessons in orbital dynamics (I'm assuming you're studying this stuff). The mass of an object cancels out when solving for its motion in a gravitational field - that's why two objects of different mass fall at the same rate, disregarding air resistance. The same holds true for orbits (which are sometimes described as "freefall that keeps missing the Earth"). Orbits in a given gravitational field are determined by the initial position and velocity vectors, and that's all. Two objects of different mass will follow identical orbits provided they both start at the same place with the same velocity.
Now, you might be thinking of the mass of the central body, in which case, yes, the field depends on that, and therefore so do the velocities of any orbiting bodies. But their velocities can't be determined from the mass of the central body alone - you need to know the details of their orbits.
If you're just limiting yourself to circular orbits, however, then all you need to know is the radius, and you can get the velocity (look at my earlier post on balancing the central force with the inertial, or centrifugal force). For example, a handy approximation for a circular orbit 7000 km from the center of the Earth is to give the object in question a velocity of 7 km/sec perpendicular to the radial vector. It's not exactly circular, but it's decent for back-of-the envelope calculations. The point is that once you have the central field, the radius alone is enough to determine the velocity in a circular orbit.
Hope that helps some,
Bruce