GRE 75, orbits, satellites and their periods

AI Thread Summary
The discussion centers on understanding the orbital mechanics of satellites, specifically the period of a hypothetical Earth satellite at sea level, which is 80 minutes, compared to a synchronous satellite that orbits every 24 hours. The key equation referenced is Kepler's third law, which states that the square of the orbital period is proportional to the cube of the semi-major axis of the orbit. By applying this law, the radius of a synchronous satellite orbit, expressed in terms of Earth's radius (Re), is determined to be approximately 7 Re. Participants express confusion about the calculations and the relationship between the periods and radii of different orbits. The final consensus confirms that the answer is indeed 7 Re, derived from the appropriate application of the formulas.
quantumworld
Messages
36
Reaction score
0
Here is a question that I am having a hard time understanding.

75) the period of a hypothetical Earth satellite orbiting at sea level would be 80 minutes. In terms of the Earth's radius Re, the radius of a synchronous satellite orbit ( period 24 hours) is mostly:
(A) 3 Re
(B) 7 Re
(C) 18 Re
(D) 320 Re
(E) 5800 Re
the answer is (B) 7 Re, but how is that, and I was surprised that it takes the Earth 24 hours to go around itself, but a satellite could make it in only 80 minutes . But most importantly is how did they get 7 Re for the answer, and I actually don't understand the question itself... :redface:

Thank u so much!
 
Physics news on Phys.org
For the 80 minutes (or 1.333hours) just think how fast something would have to be traveling around the Earth at sea level (ignore terrain) to stay in orbit (avoid crashing to the ground). It has to be crazy fast.

The ultimate equation to remember for that is that
R1^3 / T1^2 = R2^3 / T2^2

So r^3/T^2 is equal to some constant
therefor r^3 is proportional to T^2
So for the first part
Re^3 = k(constant)*(4/3 hrs)^2
solve for k
k = 9/16 Re^3

so plug that in for the higher orbit

X^3 = (9/16 Re^3) * (24 hours)^2
X^3 = (24*24*9/16)Re^3 = (1.5*24*9)Re^3 = 1.5*216*Re^3 = 324 Re^3
this is the tricky part I would guess. Its not exactly 7
you need to take the cubed root of 324. I would, here , just cube each of the answers and see wthich is the closest, which is 7 at (343).

Man am I DREADING this test in november.
 
quantumworld said:
Here is a question that I am having a hard time understanding.

75) the period of a hypothetical Earth satellite orbiting at sea level would be 80 minutes. In terms of the Earth's radius Re, the radius of a synchronous satellite orbit ( period 24 hours) is mostly:
(A) 3 Re
(B) 7 Re
(C) 18 Re
(D) 320 Re
(E) 5800 Re
the answer is (B) 7 Re, but how is that, and I was surprised that it takes the Earth 24 hours to go around itself, but a satellite could make it in only 80 minutes . But most importantly is how did they get 7 Re for the answer, and I actually don't understand the question itself... :redface:

Thank u so much!

Healey01 already provided the solution. It's important to know kepler's 3rd law: P^2 = a^3.

If we write your answer as a multiple N times Earth's radius, then we have

{ 4/3 h \over 24 h}^2 = {R_E \over N R_E}^3

which gives
18^2 = N^3 or N= 18^{2/3}. It's then easy to get the answer (for example, by writing 18^2 = 27 \times 8 \times 1.5 so the cube root is a bit more than 6).

Pat
 
Thread 'Collision of a bullet on a rod-string system: query'
In this question, I have a question. I am NOT trying to solve it, but it is just a conceptual question. Consider the point on the rod, which connects the string and the rod. My question: just before and after the collision, is ANGULAR momentum CONSERVED about this point? Lets call the point which connects the string and rod as P. Why am I asking this? : it is clear from the scenario that the point of concern, which connects the string and the rod, moves in a circular path due to the string...
Back
Top